FREGAT R/B, 41551
Orbit data source: Space-Track
FREGAT R/B, 41551 is space debris originally from a launch on Tue, 24 May 2016 UTC launched from the French Guiana (FRGUI). 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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41551 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,050 kg wet, 1,050 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Irr, 1.6 m
Radar Cross Section
11.055 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 FREGAT R/B
1 41551U 16030C 26058.92179891 .00000035 00000-0 00000-0 0 9991
2 41551 55.0147 227.9597 0021410 236.1518 123.6092 1.67596730 59792Epoch: 2026-02-27T22:07Z
TLE epoch observation values (Epoch: 2026-02-27T22:07:23.425Z)
Latitude
0.00001°
Longitude
98.36133°
Altitude
23,595.854 km
Speed
3.645 km/s
True Right ascension
15h 11m 50s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:21:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,624.109 km
Perigee altitude
23,495.914 km
Semi-major axis
29,938.148 km
Eccentricity
0.00214
Inclination
55.0147°
RAAN
227.9597°
Arg. of periapsis
236.1518°
True anomaly
123.81322°
Mean anomaly
123.6092°
Eccentric anomaly
123.71124°
Mean motion
0.41899 °/min
Orbital period
859.2 mins
BSTAR
0
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Other satellites on launch #30 in the year 2016 (2016-05-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FREGAT R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 116 mins | 2026-03-03 01:38:55.241Z | 322.996° NNW | 2026-03-03 02:36:55.241Z | 305.728° NW | 14.552° | 2026-03-03 03:34:55.241Z | 286.619° WNW |
| 178 mins | 2026-03-03 10:42:55.241Z | 189.305° SSW | 2026-03-03 13:40:55.241Z | 219.82° SW | 44.402° | 2026-03-03 13:40:55.241Z | 219.82° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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