FREGAT R/B, 47720
Orbit data source: Space-Track
FREGAT R/B, 47720 is space debris originally from a launch on Sun, 28 Feb 2021 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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47720 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: 2 days ago
TLE from 2 days ago
0 FREGAT R/B
1 47720U 21016B 26170.98627314 -.00001110 00000-0 76769-3 0 9998
2 47720 63.2573 49.1491 7410091 267.6340 14.3750 1.98977411 38497Epoch: 2026-06-19T23:40Z
TLE epoch observation values (Epoch: 2026-06-19T23:40:13.999Z)
Latitude
-0.00007°
Longitude
145.96083°
Altitude
6,068.26 km
Speed
7.009 km/s
True Right ascension
03h 16m 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
21:25:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
40,107.263 km
Perigee altitude
536.988 km
Semi-major axis
26,700.263 km
Eccentricity
0.74101
Inclination
63.2573°
RAAN
49.1491°
Arg. of periapsis
267.634°
True anomaly
92.25072°
Mean anomaly
14.375°
Eccentric anomaly
43.71633°
Mean motion
0.49747 °/min
Orbital period
723.66 mins
BSTAR
0.00076769
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Other satellites on launch #16 in the year 2021 (2021-02-28 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. |
|---|---|---|---|---|---|---|---|
| 619 mins | 2026-06-22 12:24:16.458Z | 83.71° E | 2026-06-22 18:00:16.458Z | 35.92° NE | 32.79° | 2026-06-22 22:43:16.458Z | 82.874° E |
| 373 mins | 2026-06-23 02:28:16.458Z | 323.848° NNW | 2026-06-23 05:48:16.458Z | 333.784° NNW | 16.385° | 2026-06-23 08:41:16.458Z | 328.434° NNW |
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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