FREGAT R/B, 40546
Orbit data source: Space-Track
FREGAT R/B, 40546 is space debris originally from a launch on Fri, 27 Mar 2015 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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40546 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: 2 weeks ago
TLE from 2 weeks ago
0 FREGAT R/B
1 40546U 15017C 26058.21836726 -.00000105 00000-0 00000-0 0 9996
2 40546 57.0075 348.4974 0017116 231.0577 128.7909 1.67685009 66904Epoch: 2026-02-27T05:14Z
TLE epoch observation values (Epoch: 2026-02-27T05:14:26.931Z)
Latitude
-0.00001°
Longitude
112.81741°
Altitude
23,581.969 km
Speed
3.646 km/s
True Right ascension
23h 13m 57s
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
18:46:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,600.656 km
Perigee altitude
23,498.208 km
Semi-major axis
29,927.569 km
Eccentricity
0.00171
Inclination
57.0075°
RAAN
348.4974°
Arg. of periapsis
231.0577°
True anomaly
128.94357°
Mean anomaly
128.7909°
Eccentric anomaly
128.86726°
Mean motion
0.41921 °/min
Orbital period
858.75 mins
BSTAR
0
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Other satellites on launch #17 in the year 2015 (2015-03-27 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. |
|---|---|---|---|---|---|---|---|
| 87 mins | 2026-03-10 14:51:12.482Z | 63.255° ENE | 2026-03-10 15:35:12.482Z | 48.678° ENE | 12.692° | 2026-03-10 16:18:12.482Z | 35.384° NE |
| 260 mins | 2026-03-11 06:31:12.482Z | 323.254° NNW | 2026-03-11 08:40:12.482Z | 289.944° WNW | 30.385° | 2026-03-11 10:51:12.482Z | 243.336° WSW |
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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