FREGAT R/B, 40316
Orbit data source: Space-Track
FREGAT R/B, 40316 is space debris in MEO originally from a launch on Sun, 30 Nov 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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40316 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 FREGAT R/B
1 40316U 14075B 26128.15813081 .00000023 00000-0 00000+0 0 9991
2 40316 63.5524 198.2898 0042576 137.2589 223.1428 2.08635584 87126Epoch: 2026-05-08T03:47Z
TLE epoch observation values (Epoch: 2026-05-08T03:47:42.501Z)
Latitude
-0.00001°
Longitude
-84.6306°
Altitude
19,573.804 km
Speed
3.913 km/s
True Right ascension
13h 13m 09s
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
19:21:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,602.464 km
Perigee altitude
19,382.172 km
Semi-major axis
25,870.455 km
Eccentricity
0.00426
Inclination
63.5524°
RAAN
198.2898°
Arg. of periapsis
137.2589°
True anomaly
222.81047°
Mean anomaly
223.1428°
Eccentric anomaly
222.9765°
Mean motion
0.5216 °/min
Orbital period
690.18 mins
BSTAR
0
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Other satellites on launch #75 in the year 2014 (2014-11-30 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. |
|---|---|---|---|---|---|---|---|
| 180 mins | 2026-05-08 17:58:49.886Z | 333.362° NNW | 2026-05-08 19:26:49.886Z | 295.643° NW | 27.847° | 2026-05-08 20:58:49.886Z | 249.721° W |
| 244 mins | 2026-05-09 02:11:49.886Z | 142.913° SSE | 2026-05-09 04:13:49.886Z | 80.015° E | 38.785° | 2026-05-09 06:15:49.886Z | 33.148° 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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