Near-Earth Object Close-Approach Report: June 17, 2026
On June 17, 2026, screening of the NASA NeoWs catalogue resolves 37 near-Earth object close approaches across the report window. The single closest encounter reported by NASA NEOWS is 2003 LN6, passing at approximately 3.68 lunar distances (1,417,040 km) with a relative velocity near 3.9 km/s. Its order-of-magnitude kinetic energy, for scale only, is near 0 Mt TNT equivalent; no listed object is on an impacting trajectory. Screening of Live NASA JPL CAD shows only routine safe approaches. The next closest encounter reported by NASA CAD is 2026 LO1 at just over 14 lunar distances as shown below with five objects which are approaching shortly after. A seven day outlook from NASA’s NeoWs is included for comprehensive coverage from both NASA data sets.
Next Asteroid Close Approaches (NASA CAD Data - Live at time of writing)
Live Nasa CAD Data Provenance: relay=allorigins-get / allorigins-get | CAD v1.5 | Scout v1.3 | source=CAD + SCOUT | fetched=Wed, 17 Jun 2026 23:04:01 UTC | window(TDB)=2026-06-17..2026-06-23 | dist-max=0.2056AU | validation=PASS
| Object | Epoch (UTC) | Dist (LD) | Dist (km) | v_rel | Diameter | Status |
|---|---|---|---|---|---|---|
| 2011 ET74 | 2026-Jun-18 01:05 | 148.16 | 56,976,627 | 6.9 | 0.023 | ROUTINE |
| 2018 WS | 2026-Jun-18 02:30 | 126.46 | 48,633,599 | 5.0 | 0.020 | ROUTINE |
| 2013 NG10 | 2026-Jun-18 11:07 | 138.92 | 53,425,589 | 11.2 | 0.115 | ROUTINE |
| 2002 WX12 | 2026-Jun-18 12:14 | 53.96 | 20,750,421 | 18.5 | 0.390 | ROUTINE |
| 2014 QZ295 | 2026-Jun-18 19:56 | 90.74 | 34,894,134 | 7.4 | 0.044 | ROUTINE |
| 2003 LN6 | 2026-Jun-18 20:54 | 3.68 | 1,417,040 | 3.9 | 0.045 | NOTABLE |
| 17182 (1999 VU | 2026-Jun-19 07:54 | 68.52 | 26,351,461 | 13.8 | 1.490 | ROUTINE |
| 2019 UG2 | 2026-Jun-19 18:55 | 165.95 | 63,821,319 | 11.9 | 0.055 | ROUTINE |
| 2001 MY7 | 2026-Jun-19 20:56 | 76.32 | 29,349,367 | 17.5 | 0.175 | ROUTINE |
| 2020 AP3 | 2026-Jun-20 00:31 | 85.60 | 32,918,736 | 5.6 | 0.019 | ROUTINE |
| 2014 WA201 | 2026-Jun-20 22:51 | 52.65 | 20,247,474 | 14.9 | 0.017 | ROUTINE |
| 2019 NJ5 | 2026-Jun-20 23:45 | 184.47 | 70,941,539 | 5.2 | 0.089 | ROUTINE |
| 2008 JL24 | 2026-Jun-21 00:21 | 36.19 | 13,918,263 | 2.0 | 0.005 | ROUTINE |
| 2020 BT3 | 2026-Jun-21 11:33 | 157.53 | 60,582,124 | 15.0 | 0.031 | ROUTINE |
| 470310 (2007 LB15 | 2026-Jun-21 19:53 | 81.18 | 31,218,106 | 21.5 | 0.476 | PHA |
| 2015 GF27 | 2026-Jun-21 20:38 | 117.51 | 45,191,105 | 5.3 | 0.808 | ROUTINE |
| 2016 CN248 | 2026-Jun-21 20:39 | 165.61 | 63,690,493 | 16.7 | 0.014 | ROUTINE |
| 2017 AY3 | 2026-Jun-21 22:39 | 39.78 | 15,298,790 | 14.6 | 0.295 | ROUTINE |
| 2017 FL91 | 2026-Jun-22 02:51 | 191.60 | 73,685,455 | 3.0 | 0.241 | ROUTINE |
| 2016 LC9 | 2026-Jun-22 08:09 | 24.57 | 9,447,842 | 3.4 | 0 |
Methodology
Close-approach geometry is taken from NASA NeoWs, which is fed by the Jet Propulsion Laboratory Solar System Dynamics small-body solutions that also underpin CNEOS. No local trajectory integration is performed; the report consumes NASA solutions directly to preserve the authoritative state.
- Source choice. The JPL CNEOS CAD and SBDB endpoints (ssd-api.jpl.nasa.gov) cannot be embedded in a website per NASA CORS policy, so NeoWs (api.nasa.gov) is used: it carries the same underlying JPL small-body data and is CORS enabled.
- Time scale. NeoWs reports close-approach epochs on the UTC civil scale. For reference the BCRS dynamical offset is TT - UTC = 69.184 s for 2026 (37 leap seconds plus the 32.184 s TAI-to-TT constant).
- Distance units. Miss distance is taken from NeoWs in astronomical units and lunar distances (1 au = 149,597,871 km, 1 LD = 384,400 km, IAU 2012).
- Size estimate. Diameter uses the NeoWs estimated_diameter bracket (derived from absolute magnitude H with standard albedo bounds); the geometric mean is reported.
- Energy context. Impact-energy figures are order-of-magnitude only: KE = 0.5 m v^2 with mass from the estimated diameter and an assumed bulk density of 2600 kg/m^3. They quantify scale, not risk - no listed object is on an impact trajectory.
- Validation. Every record is range-checked (0 < dist ≤ 1 au; 0.05 ≤ v_rel ≤ 100 km/s; -5 ≤ H ≤ 40) and a diameter-from-H constant self-test runs each build. Result: PASS (H=22 -> 0.106-0.237 km); flagged records: 0.
Data Provenance
Data date and time (UTC): 2026-06-17T22:52:37.725Z
Cache state: Miss (verified fresh API call)
Sources: NASA NeoWs, JPL CAD
endpoint: https://api.nasa.gov/neo/rest/v1/feed?start_date=2026-06-17&end_date=2026-06-24&api_key=***
docs: https://api.nasa.gov/
retrieved: 2026-06-17T22:52:37.858Z
Source 2: NASA NeoWs lookup
endpoint: https://api.nasa.gov/neo/rest/v1/neo/3156302?api_key=***
docs: https://api.nasa.gov/
retrieved: 2026-06-17T22:52:39.753Z
Constants:
- AU = 149597870.7 km (IAU 2012 Resolution B2)
- Lunar distance = 384400 km (JPL/IAU nominal mean)
- Earth mean radius = 6371 km (IUGG)
- TT - UTC = 69.184 s (37 leap seconds + 32.184 s), valid 2026
- Diameter self-test: D[km] = 1329 / sqrt(pv) * 10^(-H/5), pv 0.25-0.05 (Bowell)
- Impact-energy estimate: KE = 0.5 m v^2, m from D and rho = 2600 kg/m^3; 1 Mt = 4.184e15 J
Source note: JPL ssd-api (CNEOS CAD / SBDB) is intentionally called for the live upcoming close approaches because NASA NeoWs Data may be delayed or lag. This is due to NASA update frequency and not a flaw in our system. To remedy this, we provide both official sets of API data to ensure you receive the most comprehensive information.