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Showing posts with label Original Orbital Calculations. Show all posts
Showing posts with label Original Orbital Calculations. Show all posts

Newly Discovered NEO Asteroid 2026 SA8 Close Approach to Earth Orbital Report and Deterministic Analysis as it Passes Closer Than The Moon

Asteroid 2026 SA8 · Astrophyzix Scientific Close-Approach & Orbital Report

Asteroid 2026 SA8 — Small Apollo NEO Close-Approach & Orbital Profile · JPL CAD confirmed
✅ Data source: JPL Close-Approach Data (CAD) · confirmed solution, 2-day arc, updated 28 September 2026
📌 Cited and Featured by: 🔹 Google AI 🔹 Copilot Answers 🔹 Hacker News 🔹 Bing AI 🔹 News Nook 🔹 iAsk Student 🔹 Google Gemini 🔹 ChatGPT 🔹 Grok
SunPerihelion 0.818 auAphelion 1.31 auEarth · 2026 SA8approach 28 Sep 2026MercuryVenusEarthMars2026 SA8

Top-down schematic. Orbit size and shape are drawn from the published elements (a, e, q, Q); the orientation of the orbit and the marked encounter point are approximate. 2026 SA8's orbit is nearly the same size as Earth's — an Apollo that happens to cross very close to home.

Apollo NEO2-Day Data Arc11 ObservationsARI 43 / 100NO IMPACT RISK — Not on Sentry

Key Takeaways of Asteroid 2026 SA8

  • Close approach: predicted for 28 Sep 2026 at 06:45 TDB (timing uncertainty ± 22 minutes), confirmed in the JPL CAD record. The miss distance is 0.988 LD (≈ 379,868 km, 0.00254 au) — slightly closer than the Moon's own average distance from Earth (384,400 km), though still roughly 60 Earth radii out.
  • Speed: 6.61 km/s relative to Earth (≈ 23,800 km/h), the slowest of the recent tracked passes; v∞ 6.45 km/s.
  • Orbit class: Apollo NEO — a = 1.07 au, e = 0.231, i = 1.89°, orbital period ≈ 401 days (1.10 years). Its orbit is close in size to Earth's own, only about 10% longer in period.
  • Earth MOID: 0.0027 au (≈ 404,000 km). This pass, at 0.00254 au, is actually a touch closer than the nominal MOID figure — with only a 2-day arc, both numbers carry some uncertainty.
  • Size estimate: absolute magnitude H = 28.634, giving a diameter of about 6.7 m (range 5.0–11.1 m, albedo-dependent) — the smallest of the recent tracked objects. The size is H-derived, not measured.
  • Orbit quality: the solution rests on a very short 2-day data arc with just 11 observations, so the orbital elements are provisional and should be treated as preliminary.
  • Risk context: not a Potentially Hazardous Asteroid (H is far above the H ≤ 22 PHA threshold), not on the Sentry watchlist, and no Scout entry.
  • Keep it in proportion: a sub-lunar-distance flyby from a ~7 m object is a routine, expected detection for current sky surveys — small objects like this pass this close to Earth regularly and burn up harmlessly if they ever did enter the atmosphere.

Approach Scale

Earth2026 SA8 · 0.99 LDMoon · 1 LD2 LD1 LD ≈ 384,400 km

2026 SA8's flyby distance sits almost exactly at the Moon's own distance — the marker and the Moon's tick nearly overlap on this scale.

Scientific Consensus Snapshot of 2026 SA8

ParameterStatus
Orbit classApollo NEO (a > 1 au, q < 1.017 au — Earth-crossing)
Semi-major axis (a)1.07 au
Eccentricity (e)0.231
Perihelion distance (q)0.818 au
Aphelion distance (Q)1.31 au
Inclination (i)1.89°
Orbital period≈ 401 days (1.10 years)
Earth MOID0.0027 au (≈ 404,000 km)
Tisserand parameter (TJ)≈ 5.8 † — well above 3, firmly asteroidal
Absolute magnitude (H)28.634 (very small object)
Estimated diameter≈ 6.7 m (5.0–11.1 m), H-derived
Observations / data arc11 observations over 2 days
Sentry / ScoutNot on Sentry watchlist · no Scout entry
Hazard levelNon-hazardous size; not PHA-class

† Derived by Astrophyzix from a, e and i. All other values are taken from the JPL CAD/SBDB record.

2026 SA8 Close-Approach Overview

Date/Time (TDB)BodyNominal distanceMin–Max distance (au)Vrel (km/s)
2026-09-28 06:45 ± 00:22Earth0.00254 au
0.988 LD
0.00251 – 0.002576.61

Same-day company

Another small object passed later the same day (28 Sep 2026):

ObjectDate/Time (TDB)Miss distanceVelocityEst. sizeARI
2026 SX22026-09-28 18:114.102 LD7.69 km/s13 m32

1. Asteroid 2026 SA8

Small Apollo NEO on an orbit close in size to Earth's own, with a sub-lunar-distance flyby predicted for 28 September 2026 — dynamically notable for how close it comes, but non-hazardous in current solutions.

Asteroid 2026 SA8 Orbital Geometry

ParameterValue
Orbit classApollo (APO) — Earth-crossing NEO
Semi-major axis (a)1.07 au
Eccentricity (e)0.231
Perihelion distance (q)0.818 au
Aphelion distance (Q)1.31 au
Inclination (i)1.89°
Mean motion (n)≈ 0.90 deg/day †
Orbital period≈ 401 days (1.10 years)
Earth MOID0.0027 au (≈ 404,000 km)
Data arc2 days
Observations used11

Physical Characteristics of NEO 2026 SA8

ParameterValue
Absolute magnitude (H)28.634
Estimated diameter≈ 5.0–11.1 m (nominal 6.7 m, assuming albedo 0.25–0.05)
Size sourceH-derived (no radar or thermal measurement)
Rotation periodNot published
Spectral typeUnknown (no published taxonomy)
PHA classificationNo — below PHA-class threshold (derived)

2026 SA8 occupies an orbit that is, in size, almost a twin of Earth's — a = 1.07 au against Earth's 1.00 au, and a period of 401 days against Earth's 365. What makes it Earth-crossing rather than co-orbital is its eccentricity of 0.231, which carries it from 0.818 au at perihelion (between Venus and Earth) out to 1.31 au at aphelion (between Earth and Mars). At only about 5–11 m across, it is smaller than the 2013 Chelyabinsk impactor and would pose no meaningful hazard even in a hypothetical atmospheric entry.

Interpretation of the Predicted Approach

With just a 2-day arc and 11 observations, this is the most provisional of the recent orbit solutions in this series — the ± 22 minute timing uncertainty on the approach itself reflects that. Both the approach distance and the quoted Earth MOID should be read as preliminary until more astrometry comes in.

The passage at 0.988 LD is closer than the Moon's own orbit, which is a useful reminder of scale: even "close by astronomical standards" here means a clean miss tens of thousands of kilometres beyond any risk to Earth.

Astrophyzix Assessment:

The predicted 28 September 2026 approach is safe and non-hazardous. Its short data arc makes it a priority target for follow-up astrometry in the days around closest approach, both to firm up this pass and to characterise the orbit for future apparitions.

Astrophyzix Risk Index (ARI)

43 / 100 for 2026 SA8, matching 2026 SY2's score despite being far smaller and slower — driven mainly by its very tight approach distance.

ARI is an Astrophyzix composite index used to rank close approaches at a glance. It is not an official NASA, ESA or IAU hazard rating; the authoritative impact-risk sources are Sentry and Scout.

Newly Discovered NEO Asteroid 2026SC Close Approach Report, Analysis and Complete Official Data Profile - Astrophyzix Digital Observatory

Astrophyzix Scientific Close-Approach & Orbital Report NEO 2026SC Official Data

Asteroid 2026 SC — Small Aten NEO Close-Approach & Orbital Profile · JPL CAD confirmed
✅ Data source: JPL Close-Approach Data (CAD) · confirmed solution, 6-day arc
SunPerihelion 0.564 auAphelion 1.10 auEarth · 2026 SCapproach 25 Sep 2026MercuryVenusEarthMars2026 SC

Top-down schematic. Orbit size and shape are drawn from the published elements (a, e, q, Q); the orientation of the orbit and the marked encounter point are approximate. Note how small and Earth-like this orbit is compared with 2026 SY2's — 2026 SC is an Aten, spending most of its time inside Earth's orbit. 

Copyright © 2026 Astrophyzix - All images, original calculations and analysis are the digital property of Astrophyzix. No distribution without proper attribution 

Aten NEO6-Day Data Arc30 ObservationsARI 42 / 100NO IMPACT RISK — Not on Sentry

Key Takeaways of Asteroid 2026 SC

  • Close approach: predicted for 25 Sep 2026 at 13:47 TDB (timing uncertainty ± 4 minutes), confirmed in the JPL CAD record. The miss distance is 1.705 LD (≈ 655,383 km, 0.00438 au).
  • Speed: 7.75 km/s relative to Earth (≈ 27,900 km/h) — much slower than 2026 SY2's 25.1 km/s; v∞ 7.68 km/s.
  • Orbit class: Aten NEO — a = 0.832 au, e = 0.322, i = 4.66°, orbital period ≈ 277 days (0.76 years). Unlike an Apollo, an Aten spends most of its orbit inside Earth's.
  • Earth MOID: 0.0034 au (≈ 509,000 km). This pass, at 0.00438 au, is about 30% farther than the geometric MOID — not the tightest approach this orbit allows.
  • Size estimate: absolute magnitude H = 26.159, giving a diameter of about 21 m (range 15.6–34.9 m, albedo-dependent). The size is H-derived, not measured.
  • Orbit quality: the solution rests on a 6-day data arc with 30 observations — a longer baseline than a 1-day discovery arc, but still short enough that the elements are provisional.
  • Risk context: not a Potentially Hazardous Asteroid (H is above the H ≤ 22 PHA threshold), not on the Sentry watchlist, and no Scout entry.
  • Keep it in proportion: a lunar-distance-class flyby from a ~20 m object is a routine, expected detection for current sky surveys. This one is tracked, confirmed and shows no impact geometry.

Approach Scale

EarthMoon · 1 LD2026 SC · 1.71 LD2 LD1 LD ≈ 384,400 km

Scientific Consensus Snapshot of 2026 SC

ParameterStatus
Orbit classAten NEO (a < 1 au, Q > 0.983 au — Earth-crossing, orbit mostly interior to Earth's)
Semi-major axis (a)0.832 au
Eccentricity (e)0.322
Perihelion distance (q)0.564 au
Aphelion distance (Q)1.10 au
Inclination (i)4.66°
Orbital period≈ 277 days (0.76 years)
Earth MOID0.0034 au (≈ 509,000 km)
Tisserand parameter (TJ)≈ 7.0 † — well above 3, firmly asteroidal
Absolute magnitude (H)26.159 (very small object)
Estimated diameter≈ 21 m (15.6–34.9 m), H-derived
Observations / data arc30 observations over 6 days
Sentry / ScoutNot on Sentry watchlist · no Scout entry
Hazard levelNon-hazardous size; not PHA-class

† Derived by Astrophyzix from a, e and i. All other values are taken from the JPL CAD/SBDB record.

2026 SC Close-Approach Overview

Date/Time (TDB)BodyNominal distanceMin–Max distance (au)Vrel (km/s)
2026-09-25 13:47 ± 00:04Earth0.00438 au
1.705 LD
0.00437 – 0.004407.75

1. Asteroid 2026 SC

Small Aten NEO on a compact, Earth-orbit-hugging path, with a lunar-distance flyby predicted for 25 September 2026 and a tight Earth MOID — a routine, well-characterised approach with no impact geometry in current solutions.

Asteroid 2026 SC Orbital Geometry

ParameterValue
Orbit classAten (ATE) — Earth-crossing NEO
Semi-major axis (a)0.832 au
Eccentricity (e)0.322
Perihelion distance (q)0.564 au
Aphelion distance (Q)1.10 au
Inclination (i)4.66°
Longitude of node (Ω)180°
Argument of perihelion (ω)325°
Mean anomaly (M)103°
Mean motion (n)≈ 1.30 deg/day †
Orbital period≈ 277 days (0.76 years)
Earth MOID0.0034 au (≈ 509,000 km)
Data arc6 days
Observations used30

Physical Characteristics of NEO 2026 SC

ParameterValue
Absolute magnitude (H)26.159
Estimated diameter≈ 15.6–34.9 m (nominal 20.8 m, assuming albedo 0.25–0.05)
Size sourceH-derived (no radar or thermal measurement)
Rotation periodNot published
Spectral typeUnknown (no published taxonomy)
PHA classificationNo — below PHA-class threshold (derived)

2026 SC is a small Aten NEO whose orbit lies almost entirely inside Earth's, ranging from 0.564 au at perihelion (between Mercury's and Venus's distances) out to 1.10 au at aphelion, just beyond Earth's own orbit. That small overshoot at aphelion is what makes it Earth-crossing and gives it a tight MOID of 0.0034 au. At an estimated 15–35 m across, it is in the same general size class as the 2013 Chelyabinsk fireball (about 18–20 m), though it is passing at a safe distance with no impact geometry in current solutions.

Interpretation of the Predicted Approach

The 6-day data arc and 30 observations give a noticeably firmer orbit than a bare 1-day discovery arc, but the elements are still short-arc and will tighten further as more astrometry comes in before and after the 25 September pass.

Because the approach distance (0.00438 au) sits somewhat above the orbit's Earth MOID (0.0034 au), this particular encounter is not the closest geometry the orbit permits — a useful reminder that MOID describes the orbits' closest possible separation, not any single flyby.

Astrophyzix Assessment:

Astrophyzix confirms that it's predicted 25 September 2026 approach is safe, non-hazardous and a good target for follow-up astrometry. Astrophyzix Orbital calculations are consistent with NASA and no impact risk is suggested. Its Aten orbit and short period make it a candidate for early recovery in future apparitions.

Astrophyzix Risk Index (ARI)

42 / 100 for 2026 SC — close to the ARI recorded for 2026 SY2 (43) despite a much slower, more distant pass, reflecting its somewhat larger estimated size.

ARI is an Astrophyzix composite index used to rank close approaches at a glance. It is not an official NASA, ESA or IAU hazard rating; the authoritative impact-risk sources are Sentry and Scout.

ℹ️ Sources / Technical / Mathematical / Scientific / Academic / Integrators / Methods
Sources
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