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 (61 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DIAMANT R/B
1 02017U 66013B   26267.37133051  .00001340  00000-0  35130-3 0  9995
2 02017  34.0638  10.8985 1033001 130.6200 238.9004 12.93807134782626
Epoch: 2026-09-24T08:54Z
TLE epoch observation values (Epoch: 2026-09-24T08:54:42.956Z)
Latitude
-0.00001°
Longitude
-125.98956°
Altitude
1,749.5 km
Speed
6.791 km/s
True Right ascension
00h 43m 35s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
13:02:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,081.621 km
Perigee altitude
497.475 km
Semi-major axis
7,667.685 km
Eccentricity
0.1033
Inclination
34.0638°
RAAN
10.8985°
Arg. of periapsis
130.62°
True anomaly
229.44238°
Mean anomaly
238.9004°
Eccentric anomaly
234.10569°
Mean motion
3.23256 °/min
Orbital period
111.37 mins
BSTAR
0.0003513
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