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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 DIAMANT R/B
1  2017U 66013B   26088.05635804  .00002258  00000-0  59068-3 0  9999
2  2017  34.0623  86.9513 1035246  43.2687 324.4732 12.93507414759397
Epoch: 2026-03-29T01:21Z
TLE epoch observation values (Epoch: 2026-03-29T01:21:09.334Z)
Latitude
-0.00002°
Longitude
-119.80535°
Altitude
672.366 km
Speed
7.818 km/s
True Right ascension
05h 47m 48s
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
00:43:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,084.648 km
Perigee altitude
496.815 km
Semi-major axis
7,668.869 km
Eccentricity
0.10352
Inclination
34.0623°
RAAN
86.9513°
Arg. of periapsis
43.2687°
True anomaly
316.79602°
Mean anomaly
324.4732°
Eccentric anomaly
320.71771°
Mean motion
3.23181 °/min
Orbital period
111.39 mins
BSTAR
0.00059068
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