KONDOR FKA NO.2, 62138
Orbit data source: Space-Track
KONDOR FKA NO.2, 62138 is a payload satellite owned by NPO Mash (CIS) in SSO that was launched on Fri, 29 Nov 2024 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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62138 intel report (Beta)
KONDOR FKA NO.2 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 hours ago |
| Origin | |
| Manufacturer | NPOMA? |
| Mission | Operational spacecraft |
| Bus & Motor | KONDOR, Unknown motor |
| Mass | 1,050 kg wet, 1,050 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 KONDOR FKA NO.2
1 62138U 24223A 24361.12387362 .00010720 00000-0 51445-3 0 9993
2 62138 97.4389 201.4692 0002151 44.2377 315.9029 15.19047917 3985Epoch: 2024-12-26T02:58Z
Definitive object data (Epoch: 2024-12-26T02:58:22.68Z)
| Latitude | -0.00006° |
| Longitude | 61.76693° |
| Altitude | 510.741 km |
| Speed | 7.609 km/s |
| True Right ascension | 13h 25m 52s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -52.87916° |
| Longitude | -127.81045° |
| Altitude | 530.735 km |
| Speed | 7.595 km/s |
| Apparent Right ascension | 23h 06m 06s |
| Apparent Declination | -48° 54' 19" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:40:23 |
| Azimuth | 232.329° WSW |
| Elevation | -72.34° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 507.166 km |
| Perigee altitude | 504.205 km |
| Semi-major axis | 6,883.822 km |
| Eccentricity | 0.0002151 |
| Inclination | 97.4389° |
| RAAN | 201.4692° |
| Arg. of periapsis | 44.2377° |
| True anomaly | 315.88574° |
| Mean anomaly | 315.9029° |
| Eccentric anomaly | 315.89432° |
| Mean motion | 3.80013 °/min |
| BSTAR | 0.00051445 |
| Orbital period | 94.73 mins |
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Other satellites on launch #223 in the year 2024 (2024-11-29 UTC)
| KONDOR FKA NO.2, 62138 |
KONDOR FKA NO.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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-26 14:11:13.991Z | 219.712° SW | 2024-12-26 14:12:13.991Z | 246.62° WSW | 27.753° | 2024-12-26 14:15:13.991Z | 321.34° NNW |
| 4 mins | 2024-12-27 01:42:13.991Z | 66.825° ENE | 2024-12-27 01:43:13.991Z | 88.795° E | 19.889° | 2024-12-27 01:46:13.991Z | 144.993° SSE |
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