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: 12 hours ago
TLE from 12 hours ago
0 LARETS
1 27944U 03042F 25260.92893980 .00000070 00000-0 23001-4 0 9995
2 27944 98.3819 52.9668 0012651 160.5108 199.6580 14.63784288173536Epoch: 2025-09-17T22:17Z
TLE epoch observation values (Epoch: 2025-09-17T22:17:40.398Z)
Latitude
-0.00001°
Longitude
81.45063°
Altitude
692.379 km
Speed
7.506 km/s
True Right ascension
03h 31m 52s
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
02:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.993 km
Perigee altitude
669.139 km
Semi-major axis
7,056.203 km
Eccentricity
0.00127
Inclination
98.3819°
RAAN
52.9668°
Arg. of periapsis
160.5108°
True anomaly
199.6093°
Mean anomaly
199.658°
Eccentric anomaly
199.63364°
Mean motion
3.66173 °/min
Orbital period
98.31 mins
BSTAR
0.000023001
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-18 09:54:13.235Z | 149.612° SSE | 2025-09-18 09:58:13.235Z | 59.399° ENE | 40.263° | 2025-09-18 10:02:13.235Z | 355.769° N |
| 7 mins | 2025-09-18 23:29:13.235Z | 357.257° N | 2025-09-18 23:32:13.235Z | 276.028° WNW | 39.294° | 2025-09-18 23:36:13.235Z | 210.61° SW |
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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