FREGAT DEB, 46015
Orbit data source: Space-Track
FREGAT DEB, 46015 is space debris in LEO originally from a launch on Mon, 18 Jul 2011 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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46015 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 FREGAT DEB
1 46015U 11037HS 26080.19295752 .00046794 00000-0 83302-2 0 9992
2 46015 51.3519 43.0678 1286315 74.1320 299.7273 12.54861150240988Epoch: 2026-03-21T04:37Z
TLE epoch observation values (Epoch: 2026-03-21T04:37:51.529Z)
Latitude
0.00002°
Longitude
154.88592°
Altitude
1,052.643 km
Speed
7.508 km/s
True Right ascension
02h 52m 16s
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
22:27:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,450.99 km
Perigee altitude
438.457 km
Semi-major axis
7,822.861 km
Eccentricity
0.12863
Inclination
51.3519°
RAAN
43.0678°
Arg. of periapsis
74.132°
True anomaly
285.95732°
Mean anomaly
299.7273°
Eccentric anomaly
292.94014°
Mean motion
3.13686 °/min
Orbital period
114.76 mins
BSTAR
0.0083302
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Other satellites on launch #37 in the year 2011 (2011-07-18 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 DEB 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-21 23:54:41.994Z | 210.41° SW | 2026-03-21 23:57:41.994Z | 163.586° S | 34.444° | 2026-03-22 00:00:41.994Z | 70.003° E |
| 7 mins | 2026-03-22 05:56:41.994Z | 334.353° NNW | 2026-03-22 05:58:41.994Z | 32.084° NE | 33.756° | 2026-03-22 06:03:41.994Z | 102.961° ESE |
| 8 mins | 2026-03-22 07:55:41.994Z | 273.687° WNW | 2026-03-22 07:58:41.994Z | 213.118° SW | 29.987° | 2026-03-22 08:03:41.994Z | 161.206° S |
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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