ARIANE 3 R/B, 18953
Orbit data source: Space-Track
ARIANE 3 R/B, 18953 is space debris in HEO originally from a launch on Fri, 11 Mar 1988 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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18953 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 2 days ago
0 ARIANE 3 R/B
1 18953U 88018C 25205.32906329 .00000725 00000-0 14973-2 0 9999
2 18953 7.1622 31.1502 7121776 250.2582 25.0732 2.42243747317323
Epoch: 2025-07-24T07:53Z
TLE epoch observation values (Epoch: 2025-07-24T07:53:51.068Z)
Latitude
-0.00024°
Longitude
-29.38369°
Altitude
8,825.548 km
Speed
5.951 km/s
True Right ascension
02h 05m 30s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
5.70458°
Longitude
22.34724°
Altitude
29,003.778 km
Speed
2.348 km/s
Apparent Right ascension
05h 15m 03s
Apparent Declination
0° 48' 55"
Sunlit
Visualization observer readout
Local Sidereal Time
15:03:13
Azimuth
314.113° NW
Elevation
-40.738°
Doppler factor
1
Orbital elements
Apogee altitude
33,728.323 km
Perigee altitude
363.884 km
Semi-major axis
23,424.241 km
Eccentricity
0.71218
Inclination
7.1622°
RAAN
31.1502°
Arg. of periapsis
250.2582°
True anomaly
109.92807°
Mean anomaly
25.0732°
Eccentric anomaly
60.63517°
Mean motion
0.6054 °/min
Orbital period
594.64 mins
BSTAR
0.0014973
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Other satellites on launch #18 in the year 1988 (1988-03-11 UTC)
ARIANE 3 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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357 mins | 2025-07-26 11:45:37.443Z | 99.787° ESE | 2025-07-26 16:01:37.443Z | 116.524° SE | 25.417° | 2025-07-26 17:42:37.443Z | 109.705° ESE |
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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