KOMPASS, 27002
Orbit data source: Space-Track
KOMPASS, 27002 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Mon, 10 Dec 2001 UTC via a ZENIT-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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27002 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Makeev
Mission
Civil Science
Bus & Motor
SHTIL, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trunc Poly + 4 Pan, 0.4 m
Radar Cross Section
0.451 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 KOMPASS
1 27002U 01056B 25260.07110559 .00000026 00000-0 81468-4 0 9995
2 27002 99.7747 65.1325 0020170 113.8426 4.5258 13.70599917188825Epoch: 2025-09-17T01:42Z
TLE epoch observation values (Epoch: 2025-09-17T01:42:23.522Z)
Latitude
60.20566°
Longitude
-119.30126°
Altitude
992.75 km
Speed
7.368 km/s
True Right ascension
17h 30m 11s
True Declination
60° 03' 43"
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
18:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,009.567 km
Perigee altitude
979.825 km
Semi-major axis
7,372.833 km
Eccentricity
0.00202
Inclination
99.7747°
RAAN
65.1325°
Arg. of periapsis
113.8426°
True anomaly
4.54408°
Mean anomaly
4.5258°
Eccentric anomaly
4.53494°
Mean motion
3.4284 °/min
Orbital period
105.01 mins
BSTAR
0.000081468
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Other satellites on launch #56 in the year 2001 (2001-12-10 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.KOMPASS 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-18 10:32:17.835Z | 144.902° SSE | 2025-09-18 10:37:17.835Z | 75.963° E | 40.158° | 2025-09-18 10:43:17.835Z | 353.658° N |
| 7 mins | 2025-09-18 12:18:17.835Z | 229.951° WSW | 2025-09-18 12:21:17.835Z | 265.395° W | 20.093° | 2025-09-18 12:25:17.835Z | 310.021° NW |
| 9 mins | 2025-09-18 23:18:17.835Z | 41.337° NE | 2025-09-18 23:22:17.835Z | 102.447° ESE | 31.608° | 2025-09-18 23:27:17.835Z | 163.555° S |
| 9 mins | 2025-09-19 01:01:17.835Z | 350.689° N | 2025-09-19 01:05:17.835Z | 300.643° NW | 28.691° | 2025-09-19 01:10:17.835Z | 236.838° WSW |
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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