COSMOS 2227, 22284
Orbit data source: Space-Track
COSMOS 2227, 22284 is a payload satellite owned by GRU (CIS) in LEO that was launched on Fri, 25 Dec 1992 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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22284 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Yuzhnoe
Mission
Defense Sigint
Bus & Motor
TSELINA-2, Unknown motor
Mass
3,250 kg wet, 3,250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 9.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 COSMOS 2227
1 22284U 92093A 25352.94082424 -.00000253 00000-0 -10846-3 0 9995
2 22284 70.9766 201.2716 0017694 162.9893 197.1826 14.13744648701351Epoch: 2025-12-18T22:34Z
TLE epoch observation values (Epoch: 2025-12-18T22:34:47.214Z)
Latitude
0.00001°
Longitude
134.78576°
Altitude
861.2 km
Speed
7.416 km/s
True Right ascension
13h 25m 05s
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
06:06:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
857.294 km
Perigee altitude
831.735 km
Semi-major axis
7,222.651 km
Eccentricity
0.00177
Inclination
70.9766°
RAAN
201.2716°
Arg. of periapsis
162.9893°
True anomaly
197.12283°
Mean anomaly
197.1826°
Eccentric anomaly
197.1527°
Mean motion
3.53589 °/min
Orbital period
101.81 mins
BSTAR
-0.00010846
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Other satellites on launch #93 in the year 1992 (1992-12-25 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.COSMOS 2227 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-19 14:00:13.353Z | 124.655° SE | 2025-12-19 14:02:13.353Z | 102.383° ESE | 14.524° | 2025-12-19 14:05:13.353Z | 68.716° E |
| 9 mins | 2025-12-19 15:42:13.353Z | 213.771° SW | 2025-12-19 15:46:13.353Z | 308.727° NW | 43.259° | 2025-12-19 15:51:13.353Z | 18.187° NNE |
| 9 mins | 2025-12-20 00:37:13.353Z | 353.417° N | 2025-12-20 00:41:13.353Z | 64.195° ENE | 36.933° | 2025-12-20 00:46:13.353Z | 135.796° SSE |
| 6 mins | 2025-12-20 02:22:13.353Z | 295.166° NW | 2025-12-20 02:25:13.353Z | 254.328° W | 20.389° | 2025-12-20 02:28:13.353Z | 217.106° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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