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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 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.

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