ARIANE 44P R/B, 26488
Orbit data source: Space-Track
ARIANE 44P R/B, 26488 is space debris in HEO originally from a launch on Wed, 06 Sep 2000 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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26488 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ARIANE 44P R/B
1 26488U 00052B 25249.81690536 .00001145 00000-0 17009-2 0 9995
2 26488 7.3745 66.9798 7187300 198.6232 107.6350 2.34103007206996
Epoch: 2025-09-06T19:36Z
TLE epoch observation values (Epoch: 2025-09-06T19:36:20.623Z)
Latitude
0.00001°
Longitude
146.83265°
Altitude
29,957.264 km
Speed
2.303 km/s
True Right ascension
04h 28m 15s
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
11:28:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,809.65 km
Perigee altitude
362.24 km
Semi-major axis
23,964.082 km
Eccentricity
0.71873
Inclination
7.3745°
RAAN
66.9798°
Arg. of periapsis
198.6232°
True anomaly
161.50771°
Mean anomaly
107.635°
Eccentric anomaly
136.1589°
Mean motion
0.58506 °/min
Orbital period
615.32 mins
BSTAR
0.0017009
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Other satellites on launch #52 in the year 2000 (2000-09-06 UTC)
ARIANE 44P R/B Visibility forecast
Observer location: undefined°, undefined°
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. |
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553 mins | 2025-09-08 10:07:28.206Z | 213.854° SW | 2025-09-08 13:46:28.206Z | 196.991° SSW | 34.74° | 2025-09-08 19:20:28.206Z | 177.217° S |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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