OBJECT A, 55009
Orbit data source: Space-Track
OBJECT A, 55009 is a satellite in SSO that was launched on Tue, 03 Jan 2023 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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Identifier
Orbit
Country
TBDRelated business
Scanway Space (PL)Manufacturer
German Orb Sys
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 OBJECT A
1 55009U 23001A 26124.82150156 .00014113 00000-0 33890-3 0 9994
2 55009 97.3194 189.1438 0004175 265.7063 94.3707 15.41454633185543Epoch: 2026-05-04T19:42Z
TLE epoch observation values (Epoch: 2026-05-04T19:42:57.734Z)
Latitude
-0.00004°
Longitude
30.69805°
Altitude
445.155 km
Speed
7.645 km/s
True Right ascension
12h 36m 34s
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
07:39:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.595 km
Perigee altitude
435.903 km
Semi-major axis
6,816.886 km
Eccentricity
0.00042
Inclination
97.3194°
RAAN
189.1438°
Arg. of periapsis
265.7063°
True anomaly
94.4184°
Mean anomaly
94.3707°
Eccentric anomaly
94.39455°
Mean motion
3.85624 °/min
Orbital period
93.36 mins
BSTAR
0.0003389
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Other satellites on launch #1 in the year 2023 (2023-01-03 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 A 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-05 03:39:28.485Z | 115.027° SE | 2026-05-05 03:41:28.485Z | 67.004° ENE | 21.55° | 2026-05-05 03:43:28.485Z | 23.263° NE |
| 4 mins | 2026-05-05 16:33:28.485Z | 60.867° ENE | 2026-05-05 16:34:28.485Z | 88.008° E | 23.254° | 2026-05-05 16:37:28.485Z | 154.309° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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