METEOR 2-11, 15099
Orbit data source: Space-Track
METEOR 2-11, 15099 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Thu, 05 Jul 1984 UTC via a TSIKLON-3 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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15099 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Civil Weather
Bus & Motor
METEOR-2, Unknown motor
Mass
~1,500 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 2.3 m
Radar Cross Section
5.718 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 METEOR 2-11
1 15099U 84072A 25260.96533716 .00000062 00000-0 41235-4 0 9997
2 15099 82.5265 256.2622 0014232 131.4269 228.8118 13.85271872 82652Epoch: 2025-09-17T23:10Z
TLE epoch observation values (Epoch: 2025-09-17T23:10:05.13Z)
Latitude
0.00005°
Longitude
-88.39289°
Altitude
955.024 km
Speed
7.371 km/s
True Right ascension
17h 05m 02s
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
03:23:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
952.817 km
Perigee altitude
931.98 km
Semi-major axis
7,320.535 km
Eccentricity
0.00142
Inclination
82.5265°
RAAN
256.2622°
Arg. of periapsis
131.4269°
True anomaly
228.68921°
Mean anomaly
228.8118°
Eccentric anomaly
228.75049°
Mean motion
3.4652 °/min
Orbital period
103.89 mins
BSTAR
0.000041235
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Other satellites on launch #72 in the year 1984 (1984-07-05 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.METEOR 2-11 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 11:53:24.102Z | 347.92° N | 2025-09-18 11:58:24.102Z | 273.347° WNW | 43.959° | 2025-09-18 12:04:24.102Z | 181.211° SSW |
| 8 mins | 2025-09-18 23:34:24.102Z | 134.085° SE | 2025-09-18 23:37:24.102Z | 93.442° ESE | 26.711° | 2025-09-18 23:42:24.102Z | 31.373° NE |
| 9 mins | 2025-09-19 01:18:24.102Z | 226.955° WSW | 2025-09-19 01:22:24.102Z | 285.77° WNW | 30.989° | 2025-09-19 01:27:24.102Z | 348.819° N |
| 7 mins | 2025-09-19 10:26:24.102Z | 30.072° NE | 2025-09-19 10:29:24.102Z | 67.278° ENE | 21.996° | 2025-09-19 10:33:24.102Z | 116.534° SE |
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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