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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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: 9 hours ago
TLE from 9 hours ago
0 KOMPASS
1 27002U 01056B 26150.47044480 .00000023 00000-0 78407-4 0 9993
2 27002 99.7954 324.9358 0019473 177.4227 207.4401 13.70639830223818Epoch: 2026-05-30T11:17Z
TLE epoch observation values (Epoch: 2026-05-30T11:17:26.430Z)
Latitude
24.40177°
Longitude
-96.87921°
Altitude
1,012.888 km
Speed
7.341 km/s
True Right ascension
21h 21m 52s
True Declination
24° 16' 38"
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
05:27:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.91 km
Perigee altitude
980.197 km
Semi-major axis
7,372.691 km
Eccentricity
0.00195
Inclination
99.7954°
RAAN
324.9358°
Arg. of periapsis
177.4227°
True anomaly
207.33749°
Mean anomaly
207.4401°
Eccentric anomaly
207.38877°
Mean motion
3.4285 °/min
Orbital period
105 mins
BSTAR
0.000078407
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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 | 2026-05-31 00:01:22.608Z | 26.731° NE | 2026-05-31 00:07:22.608Z | 107.202° ESE | 36.721° | 2026-05-31 00:12:22.608Z | 172.176° S |
| 7 mins | 2026-05-31 01:47:22.608Z | 337.826° N | 2026-05-31 01:50:22.608Z | 298.003° NW | 24.366° | 2026-05-31 01:54:22.608Z | 249.129° W |
| 7 mins | 2026-05-31 10:07:22.608Z | 95.145° ESE | 2026-05-31 10:10:22.608Z | 60.742° ENE | 19.697° | 2026-05-31 10:14:22.608Z | 17.584° NNE |
| 11 mins | 2026-05-31 11:48:22.608Z | 176.963° S | 2026-05-31 11:53:22.608Z | 253.029° W | 42.422° | 2026-05-31 11:59:22.608Z | 338.937° N |
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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