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: 12 hours ago

TLE from 12 hours ago
0 DIAMANT R/B
1 02017U 66013B   26315.91725091  .00002665  00000-0  69943-3 0  9990
2 02017  34.0589 155.3207 1032007  86.7939 285.0041 12.93987859788913
Epoch: 2026-11-11T22:00Z
TLE epoch observation values (Epoch: 2026-11-11T22:00:50.478Z)
Latitude
-0.00003°
Longitude
134.05211°
Altitude
1,158.672 km
Speed
7.335 km/s
True Right ascension
10h 21m 16s
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
05:59:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,080.072 km
Perigee altitude
497.598 km
Semi-major axis
7,666.972 km
Eccentricity
0.1032
Inclination
34.0589°
RAAN
155.3207°
Arg. of periapsis
86.7939°
True anomaly
273.27014°
Mean anomaly
285.0041°
Eccentric anomaly
279.16665°
Mean motion
3.23301 °/min
Orbital period
111.35 mins
BSTAR
0.00069943
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