COSMOS 2024 (ETALON 2), 20026
Orbit data source: Space-Track
COSMOS 2024 (ETALON 2), 20026 is a payload satellite owned by NPO PM (CIS) in MEO that was launched on Wed, 31 May 1989 UTC via a PROTON-K/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payloads include a variety of satellites, spacecraft, and rockets 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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20026 intel report (Beta)
COSMOS 2024 (ETALON 2) details
Identifier | |
Orbit | MEO |
Last TLE update | 18 hours ago |
Origin | |
Manufacturer | NPO PM |
Mission | Operational Defense Geodetic |
Bus & Motor | ETALON, Unknown motor |
Mass | 1,230 kg wet, 1,230 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Sphere, 1.29 m |
Radar Cross Section | 1.307 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 COSMOS 2024 (ETALON 2)
1 20026U 89039C 25025.07633980 -.00000065 00000-0 00000-0 0 9991
2 20026 65.2308 327.9872 0019855 216.2907 155.1429 2.13204440277675
Epoch: 2025-01-25T01:49Z
Definitive object data (Epoch: 2025-01-25T01:49:55.758Z)
Latitude | 10.46777° |
Longitude | -179.25964° |
Altitude | 19,167.525 km |
Speed | 3.947 km/s |
True Right ascension | 22h 11m 24s |
True Declination | 10° 27' 02" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -46.02125° |
Longitude | 24.33077° |
Altitude | 19,089.688 km |
Speed | 3.96 km/s |
Apparent Right ascension | 11h 15m 15s |
Apparent Declination | -45° 41' 59" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 21:20:39 |
Azimuth | 245.071° WSW |
Elevation | -68.329° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 19,171.952 km |
Perigee altitude | 19,070.694 km |
Semi-major axis | 25,499.46 km |
Eccentricity | 0.0019855 |
Inclination | 65.2308° |
RAAN | 327.9872° |
Arg. of periapsis | 216.2907° |
True anomaly | 155.23833° |
Mean anomaly | 155.1429° |
Eccentric anomaly | 155.19063° |
Mean motion | 0.53302 °/min |
BSTAR | Unknown |
Orbital period | 675.39 mins |
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Other satellites on launch #39 in the year 1989 (1989-05-31 UTC)
COSMOS 2024 (ETALON 2) Visibility forecast
Observer location: undefined°, undefined
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. |
---|---|---|---|---|---|---|---|
374 mins | 2025-01-25 23:48:37.305Z | 239.57° WSW | 2025-01-26 03:09:37.305Z | 16.729° NNE | 40.129° | 2025-01-26 06:02:37.305Z | 133.563° SE |
Authenticating...
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