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, 1.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 DIAMANT R/B
1 02017U 66013B   26207.16651760  .00000929  00000-0  24637-3 0  9990
2 02017  34.0622 278.2106 1034146  98.6276 273.2704 12.93720591774824
Epoch: 2026-07-26T03:59Z
TLE epoch observation values (Epoch: 2026-07-26T03:59:47.120Z)
Latitude
0.00003°
Longitude
-85.60404°
Altitude
1,322.335 km
Speed
7.181 km/s
True Right ascension
18h 32m 50s
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
03:27:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,082.876 km
Perigee altitude
496.904 km
Semi-major axis
7,668.027 km
Eccentricity
0.10341
Inclination
34.0622°
RAAN
278.2106°
Arg. of periapsis
98.6276°
True anomaly
261.43615°
Mean anomaly
273.2704°
Eccentric anomaly
267.35151°
Mean motion
3.23235 °/min
Orbital period
111.37 mins
BSTAR
0.00024637
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