DIAMANT R/B, 2017

Orbit data source: Space-Track

DIAMANT R/B, 2017 is space debris in LEO originally from a launch on Thu, 17 Feb 1966 UTC launched from the Hamma Guira Space Track Range (HGSTR). 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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Identifier
2017, 1966-013B
Orbit
LEO
Country
Flag of FRFR
Related business
Manufacturer
Sud
Mission
Spacecraft
Bus & Motor
RUBIS, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
1966-02-17 (60 years ago)
Launch vehicle
Unknown
Launch site
Hamma Guira Space Track Range (HGSTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
1.347 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 DIAMANT R/B
1 02017U 66013B   25245.80116920  .00002292  00000-0  60013-3 0  9999
2 02017  34.0627 285.6146 1041464 136.0930 232.7376 12.92046579732566
Epoch: 2025-09-02T19:13Z
TLE epoch observation values (Epoch: 2025-09-02T19:13:41.018Z)
Latitude
-0°
Longitude
15.00649°
Altitude
1,823.919 km
Speed
6.729 km/s
True Right ascension
19h 02m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:46:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,095.794 km
Perigee altitude
497.221 km
Semi-major axis
7,674.644 km
Eccentricity
0.10415
Inclination
34.0627°
RAAN
285.6146°
Arg. of periapsis
136.093°
True anomaly
223.96916°
Mean anomaly
232.7376°
Eccentric anomaly
228.28345°
Mean motion
3.22817 °/min
Orbital period
111.52 mins
BSTAR
0.00060013
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