METEOR 2-1, 8026
Orbit data source: Space-Track
METEOR 2-1, 8026 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Fri, 11 Jul 1975 UTC via a VOSTOK 8A92M 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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8026 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Spacecraft
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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 METEOR 2-1
1 8026U 75064A 26171.31772135 .00000130 00000-0 65301-4 0 9997
2 8026 81.2792 20.2252 0021330 207.8613 152.1418 14.10813363619789Epoch: 2026-06-20T07:37Z
TLE epoch observation values (Epoch: 2026-06-20T07:37:31.124Z)
Latitude
-0.00003°
Longitude
-2.68856°
Altitude
873.144 km
Speed
7.409 km/s
True Right ascension
01h 20m 54s
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
23:07:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
869.187 km
Perigee altitude
838.335 km
Semi-major axis
7,231.898 km
Eccentricity
0.00213
Inclination
81.2792°
RAAN
20.2252°
Arg. of periapsis
207.8613°
True anomaly
152.25575°
Mean anomaly
152.1418°
Eccentric anomaly
152.1988°
Mean motion
3.52911 °/min
Orbital period
102.01 mins
BSTAR
0.000065301
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Other satellites on launch #64 in the year 1975 (1975-07-11 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 2-1 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-22 14:11:34.327Z | 171.9° S | 2026-06-22 14:16:34.327Z | 110.706° ESE | 40.092° | 2026-06-22 14:21:34.327Z | 19.522° NNE |
| 6 mins | 2026-06-22 15:57:34.327Z | 258.511° W | 2026-06-22 16:00:34.327Z | 295.016° NW | 17.607° | 2026-06-22 16:03:34.327Z | 329.87° NNW |
| 9 mins | 2026-06-23 00:53:34.327Z | 11.92° NNE | 2026-06-23 00:57:34.327Z | 76.898° E | 33.26° | 2026-06-23 01:02:34.327Z | 144.371° SSE |
| 7 mins | 2026-06-23 02:37:34.327Z | 309.748° NW | 2026-06-23 02:40:34.327Z | 266.799° W | 22.063° | 2026-06-23 02:44:34.327Z | 220.535° 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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