FREGAT R/B, 40130
Orbit data source: Space-Track
FREGAT R/B, 40130 is space debris in HEO originally from a launch on Fri, 22 Aug 2014 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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40130 intel report (Beta)
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Edit Public Description
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 days ago
TLE from 2 days ago
0 FREGAT R/B
1 40130U 14050C 25256.91014686 .00000047 00000-0 00000-0 0 9994
2 40130 48.5717 230.9914 2611591 213.4397 126.9824 2.05031082 82850Epoch: 2025-09-13T21:50Z
TLE epoch observation values (Epoch: 2025-09-13T21:50:36.688Z)
Latitude
-0.00002°
Longitude
-89.81048°
Altitude
24,802.396 km
Speed
3.215 km/s
True Right ascension
15h 23m 54s
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
10:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
26,630.712 km
Perigee altitude
12,959.858 km
Semi-major axis
26,173.422 km
Eccentricity
0.26116
Inclination
48.5717°
RAAN
230.9914°
Arg. of periapsis
213.4397°
True anomaly
146.57127°
Mean anomaly
126.9824°
Eccentric anomaly
137.15728°
Mean motion
0.51257 °/min
Orbital period
702.34 mins
BSTAR
0
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Other satellites on launch #50 in the year 2014 (2014-08-22 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. |
|---|---|---|---|---|---|---|---|
| 418 mins | 2025-09-15 19:27:19.340Z | 149.561° SSE | 2025-09-15 23:20:19.340Z | 89.678° E | 40.929° | 2025-09-16 02:25:19.340Z | 63.546° ENE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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