OBJECT BE, 43810
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT BE, 43810 is a satellite in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43810 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Non-operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT BE
1 43810U 18099BE 25299.64397231 .00004815 00000-0 31192-3 0 9992
2 43810 97.4236 342.2800 0009310 72.8767 287.3481 15.08548521376770Epoch: 2025-10-26T15:27Z
TLE epoch observation values (Epoch: 2025-10-26T15:27:19.207Z)
Latitude
-0°
Longitude
75.19276°
Altitude
541.793 km
Speed
7.592 km/s
True Right ascension
22h 49m 07s
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
20:41:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
544.055 km
Perigee altitude
531.178 km
Semi-major axis
6,915.753 km
Eccentricity
0.00093
Inclination
97.4236°
RAAN
342.28°
Arg. of periapsis
72.8767°
True anomaly
287.24623°
Mean anomaly
287.3481°
Eccentric anomaly
287.29717°
Mean motion
3.77384 °/min
Orbital period
95.39 mins
BSTAR
0.00031192
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Other satellites on launch #99 in the year 2018 (2018-12-03 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 BE 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 | 2025-10-27 02:44:01.171Z | 147.949° SSE | 2025-10-27 02:47:01.171Z | 59.374° ENE | 38.618° | 2025-10-27 02:50:01.171Z | 359.496° N |
| 5 mins | 2025-10-27 15:55:01.171Z | 7.718° NNE | 2025-10-27 15:57:01.171Z | 275.044° WNW | 44.676° | 2025-10-27 16:00:01.171Z | 196.822° SSW |
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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