FREGAT R/B, 40002

Orbit data source: Space-Track

FREGAT R/B, 40002 is space debris in MEO originally from a launch on Sat, 14 Jun 2014 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
40002, 2014-032B
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
2014-06-14 (12 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FREGAT R/B
1 40002U 14032B   26060.37910798 -.00000059  00000-0  00000-0 0  9999
2 40002  65.4893 323.4309 0079581  85.3873 275.5670  2.09160757 89478
Epoch: 2026-03-01T09:05Z
TLE epoch observation values (Epoch: 2026-03-01T09:05:54.929Z)
Latitude
-0.00002°
Longitude
27.77026°
Altitude
19,431.568 km
Speed
3.931 km/s
True Right ascension
21h 33m 44s
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
06:43:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,654.461 km
Perigee altitude
19,243.392 km
Semi-major axis
25,827.064 km
Eccentricity
0.00796
Inclination
65.4893°
RAAN
323.4309°
Arg. of periapsis
85.3873°
True anomaly
274.65853°
Mean anomaly
275.567°
Eccentric anomaly
275.11285°
Mean motion
0.52291 °/min
Orbital period
688.45 mins
BSTAR
0
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Other satellites on launch #32 in the year 2014 (2014-06-14 UTC)

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