LARETS, 27944
Orbit data source: Space-Track
LARETS, 27944 is a payload satellite owned by NII KP (CIS) in SSO that was launched on Sat, 27 Sep 2003 UTC via a KOSMOS 11K65M launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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27944 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NII KP
Mission
Operational Defense Calibration
Bus & Motor
Unknown
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere, 0.1 m
Radar Cross Section
0.031 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 LARETS
1 27944U 03042F 25353.89253620 .00000027 00000-0 14752-4 0 9990
2 27944 98.3903 147.5754 0011268 232.2605 127.7576 14.63822348187137Epoch: 2025-12-19T21:25Z
TLE epoch observation values (Epoch: 2025-12-19T21:25:15.127Z)
Latitude
-0.00005°
Longitude
97.53521°
Altitude
688.72 km
Speed
7.509 km/s
True Right ascension
09h 50m 18s
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
04:10:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
685.895 km
Perigee altitude
669.993 km
Semi-major axis
7,056.081 km
Eccentricity
0.00113
Inclination
98.3903°
RAAN
147.5754°
Arg. of periapsis
232.2605°
True anomaly
127.8596°
Mean anomaly
127.7576°
Eccentric anomaly
127.80861°
Mean motion
3.66183 °/min
Orbital period
98.31 mins
BSTAR
0.000014752
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Other satellites on launch #42 in the year 2003 (2003-09-27 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.LARETS 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-20 10:40:21.097Z | 182.24° SSW | 2025-12-20 10:43:21.097Z | 244.236° WSW | 41.054° | 2025-12-20 10:47:21.097Z | 337.344° NNW |
| 7 mins | 2025-12-20 22:37:21.097Z | 43.498° NE | 2025-12-20 22:40:21.097Z | 97.671° ESE | 26.946° | 2025-12-20 22:44:21.097Z | 158.76° S |
| 5 mins | 2025-12-21 00:15:21.097Z | 331.196° NNW | 2025-12-21 00:17:21.097Z | 295.025° NW | 23.363° | 2025-12-21 00:20:21.097Z | 244.984° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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