OBJECT P, 101124
Orbit data source: Space-Track
OBJECT P, 101124 is a satellite in LEO that was launched on Tue, 20 Oct 2026 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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101124 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT P
1 A1124U 26237P 26296.91668981 .00046934 00000-0 44835-2 0 9993
2 A1124 52.9883 307.6495 0006639 250.5625 102.1371 14.92818360 1387Epoch: 2026-10-23T22:00Z
TLE epoch observation values (Epoch: 2026-10-23T22:00:01.999Z)
Latitude
-5.87725°
Longitude
-59.11568°
Altitude
591.946 km
Speed
7.564 km/s
True Right ascension
20h 12m 53s
True Declination
-5° 50' 29"
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
05:37:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.058 km
Perigee altitude
584.807 km
Semi-major axis
6,967.569 km
Eccentricity
0.00066
Inclination
52.9883°
RAAN
307.6495°
Arg. of periapsis
250.5625°
True anomaly
102.21146°
Mean anomaly
102.1371°
Eccentric anomaly
102.17428°
Mean motion
3.73182 °/min
Orbital period
96.47 mins
BSTAR
0.0044835
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Other satellites on launch #237 in the year 2026 (2026-10-20 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-24 11:25:32.115Z | 290.546° WNW | 2026-10-24 11:29:32.115Z | 219.649° SW | 31.425° | 2026-10-24 11:32:32.115Z | 169.889° S |
| 7 mins | 2026-10-25 03:07:32.115Z | 213.878° SW | 2026-10-25 03:10:32.115Z | 154.595° SSE | 61.52° | 2026-10-25 03:14:32.115Z | 57.199° ENE |
| 5 mins | 2026-10-25 04:49:32.115Z | 293.619° NW | 2026-10-25 04:51:32.115Z | 335.508° NNW | 27.837° | 2026-10-25 04:54:32.115Z | 28.172° NE |
| 4 mins | 2026-10-25 08:13:32.115Z | 351.848° N | 2026-10-25 08:14:32.115Z | 9.155° NNE | 19.603° | 2026-10-25 08:17:32.115Z | 58.485° ENE |
| 6 mins | 2026-10-25 09:53:32.115Z | 319.481° NNW | 2026-10-25 09:56:32.115Z | 73.472° E | 62.032° | 2026-10-25 09:59:32.115Z | 118.396° SE |
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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