SPEKTR R, 37755
Orbit data source: Space-Track
SPEKTR R, 37755 is a Commonwealth of Independent States-origin payload satellite in HEO that was launched on Mon, 18 Jul 2011 UTC via a ZENIT-3SLBF 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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37755 intel report (Beta)
SPEKTR R details
Identifier | |
Orbit | HEO |
Last TLE update | 2 weeks ago |
Origin | |
Manufacturer | Lavochkin |
Mission | Non-operational Civil Astronomy |
Bus & Motor | NAVIGATOR, Unknown motor |
Mass | 3,660 kg wet, ~3,160 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 2 Pan + 1 Dish, 18 m |
Radar Cross Section | 18.197 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 2 weeks ago
0 SPEKTR R
1 37755U 11037A 25015.02642919 -.00010987 00000-0 00000-0 0 9991
2 37755 71.8607 337.2683 8011902 318.2818 358.4693 0.09928821 5330
Epoch: 2025-01-15T00:38Z
Definitive object data (Epoch: 2025-01-15T00:38:03.482Z)
Latitude | -18.14909° |
Longitude | -153.98593° |
Altitude | 30,341.344 km |
Speed | 4.437 km/s |
True Right ascension | 22h 01m 00s |
True Declination | -18° 07' 46" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 73.61126° |
Longitude | -67.81669° |
Altitude | 130,076.367 km |
Speed | 1.954 km/s |
Apparent Right ascension | 04h 13m 13s |
Apparent Declination | 72° 32' 50" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 20:54:55 |
Azimuth | 19.542° NNE |
Elevation | 32.348° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 348,459.011 km |
Perigee altitude | 32,787.689 km |
Semi-major axis | 197,001.487 km |
Eccentricity | 0.8011902 |
Inclination | 71.8607° |
RAAN | 337.2683° |
Arg. of periapsis | 318.2818° |
True anomaly | 337.36189° |
Mean anomaly | 358.4693° |
Eccentric anomaly | 352.39074° |
Mean motion | 0.02482 °/min |
BSTAR | Unknown |
Orbital period | 14503.19 mins |
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Other satellites on launch #37 in the year 2011 (2011-07-18 UTC)
SPEKTR R 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. |
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1440 mins | 2025-01-25 19:33:58.025Z | 19.543° NNE | 2025-01-26 05:36:58.025Z | 356.512° N | 40.322° | 2025-01-26 19:33:58.025Z | 6.847° NNE |
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