ARIANE 44LP+ R/B, 22913
Orbit data source: Space-Track
ARIANE 44LP+ R/B, 22913 is space debris in LEO originally from a launch on Sat, 20 Nov 1993 UTC launched from the French Guiana (FRGUI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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22913 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ARIANE 44LP+ R/B
1 22913U 93073C 26266.02532513 .00226505 -13879-4 11932-2 0 9993
2 22913 6.7336 161.7849 1197235 304.8511 44.4720 13.38856144726559Epoch: 2026-09-23T00:36Z
TLE epoch observation values (Epoch: 2026-09-23T00:36:28.091Z)
Latitude
0.00001°
Longitude
150.78554°
Altitude
530.792 km
Speed
7.888 km/s
True Right ascension
10h 47m 08s
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
15:21:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,017.07 km
Perigee altitude
221.799 km
Semi-major axis
7,497.572 km
Eccentricity
0.11972
Inclination
6.7336°
RAAN
161.7849°
Arg. of periapsis
304.8511°
True anomaly
55.16291°
Mean anomaly
44.472°
Eccentric anomaly
49.70394°
Mean motion
3.3432 °/min
Orbital period
107.68 mins
BSTAR
0.0011932
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Other satellites on launch #73 in the year 1993 (1993-11-20 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.ARIANE 44LP+ R/B Visibility
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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. |
|---|---|---|---|---|---|---|---|
| ARIANE 44LP+ R/B is likely not visible in the next few days. |
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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