OBJECT P, 66306
Orbit data source: Space-Track
OBJECT P, 66306 is a satellite in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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66306 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Com/MetRO
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 OBJECT P
1 66306U 25248P 26294.88563773 .00019263 00000-0 63673-3 0 9991
2 66306 45.4008 145.3158 0007890 74.0857 286.0903 15.31123562 53999Epoch: 2026-10-21T21:15Z
TLE epoch observation values (Epoch: 2026-10-21T21:15:19.099Z)
Latitude
-0.00001°
Longitude
156.15775°
Altitude
471.008 km
Speed
7.633 km/s
True Right ascension
09h 41m 15s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:29:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.409 km
Perigee altitude
468.597 km
Semi-major axis
6,852.14 km
Eccentricity
0.00079
Inclination
45.4008°
RAAN
145.3158°
Arg. of periapsis
74.0857°
True anomaly
286.00341°
Mean anomaly
286.0903°
Eccentric anomaly
286.04686°
Mean motion
3.82652 °/min
Orbital period
94.08 mins
BSTAR
0.00063673
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Other satellites on launch #248 in the year 2025 (2025-11-02 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT P Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-22 21:07:35.414Z | 301.311° NW | 2026-10-22 21:10:35.414Z | 359.959° N | 38.104° | 2026-10-22 21:13:35.414Z | 76.215° E |
| 5 mins | 2026-10-22 22:47:35.414Z | 286.569° WNW | 2026-10-22 22:49:35.414Z | 196.602° SSW | 69.955° | 2026-10-22 22:52:35.414Z | 125.537° SE |
| 6 mins | 2026-10-23 17:19:35.414Z | 236.541° WSW | 2026-10-23 17:21:35.414Z | 213.148° SW | 64.108° | 2026-10-23 17:25:35.414Z | 67.451° ENE |
| 5 mins | 2026-10-23 18:58:35.414Z | 291.686° WNW | 2026-10-23 19:00:35.414Z | 343.623° N | 37.257° | 2026-10-23 19:03:35.414Z | 56.092° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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