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, 2.5 m
Radar Cross Section
11.055 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FREGAT R/B
1 41551U 16030C 26269.54035816 .00000012 00000-0 00000-0 0 9996
2 41551 54.9475 222.3560 0022732 241.3222 118.4077 1.67596779 63323Epoch: 2026-09-26T12:58Z
TLE epoch observation values (Epoch: 2026-09-26T12:58:06.945Z)
Latitude
0.00003°
Longitude
22.46296°
Altitude
23,592.73 km
Speed
3.645 km/s
True Right ascension
14h 49m 21s
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
19:12:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,628.063 km
Perigee altitude
23,491.952 km
Semi-major axis
29,938.145 km
Eccentricity
0.00227
Inclination
54.9475°
RAAN
222.356°
Arg. of periapsis
241.3222°
True anomaly
118.63651°
Mean anomaly
118.4077°
Eccentric anomaly
118.52214°
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. |
|---|---|---|---|---|---|---|---|
| 69 mins | 2026-09-28 12:09:56.172Z | 320.058° NNW | 2026-09-28 12:43:56.172Z | 309.676° NW | 11.756° | 2026-09-28 13:18:56.172Z | 298.368° NW |
| 289 mins | 2026-09-28 20:56:56.172Z | 194.239° SSW | 2026-09-29 00:29:56.172Z | 302.862° NW | 82.213° | 2026-09-29 01:45:56.172Z | 34.66° NE |
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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