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: 19 hours ago
TLE from 19 hours ago
0 ARIANE 44LP+ R/B
1 22913U 93073C 26086.10092847 .00242435 -10275-4 17889-2 0 9997
2 22913 6.7357 64.1333 1567198 159.8752 207.0756 12.53762340703179Epoch: 2026-03-27T02:25Z
TLE epoch observation values (Epoch: 2026-03-27T02:25:20.219Z)
Latitude
-0°
Longitude
-156.74133°
Altitude
2,570.506 km
Speed
6.18 km/s
True Right ascension
04h 16m 31s
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
02:25:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,682.059 km
Perigee altitude
226.992 km
Semi-major axis
7,832.663 km
Eccentricity
0.15672
Inclination
6.7357°
RAAN
64.1333°
Arg. of periapsis
159.8752°
True anomaly
200.13741°
Mean anomaly
207.0756°
Eccentric anomaly
203.4957°
Mean motion
3.13097 °/min
Orbital period
114.98 mins
BSTAR
0.0017889
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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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