ARIANE 5 R/B, 42952
Orbit data source: Space-Track
ARIANE 5 R/B, 42952 is space debris in HEO originally from a launch on Fri, 29 Sep 2017 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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42952 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
13 hours ago
Origin
Manufacturer
ArianeGroup
Mission
Spacecraft
Bus & Motor
ESC-A, Unknown motor
Mass
~5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 3.5 m
Radar Cross Section
41.627 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 13 hours ago
0 ARIANE 5 R/B
1 42952U 17059C 25199.42220003 .00009494 00000-0 14914-2 0 9990
2 42952 6.3347 23.9560 7142353 71.9352 349.4320 2.47030804 66739Epoch: 2025-07-18T10:07Z
TLE epoch observation values (Epoch: 2025-07-18T10:07:58.082Z)
Latitude
-0.00029°
Longitude
-64.36772°
Altitude
2,859.367 km
Speed
8.309 km/s
True Right ascension
01h 36m 23s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
-5.39927°
Longitude
173.54274°
Altitude
30,505.199 km
Speed
2.09 km/s
Apparent Right ascension
17h 58m 36s
Apparent Declination
-11° 49' 10"
Sunlit
Visualization observer readout
Local Sidereal Time
12:16:11
Azimuth
101.876° ESE
Elevation
-4.239°
Doppler factor
1
Orbital elements
Apogee altitude
33,256.447 km
Perigee altitude
228.987 km
Semi-major axis
23,120.854 km
Eccentricity
0.71424
Inclination
6.3347°
RAAN
23.956°
Arg. of periapsis
71.9352°
True anomaly
288.70871°
Mean anomaly
349.432°
Eccentric anomaly
327.36°
Mean motion
0.61736 °/min
Orbital period
583.13 mins
BSTAR
0.0014914
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Other satellites on launch #59 in the year 2017 (2017-09-29 UTC)
ARIANE 5 R/B Visibility
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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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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Authenticating...
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