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 | 10 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 10 hours ago
0 KONDOR FKA NO.2
1 62138U 24223A 25024.16755298 .00028073 00000-0 13144-2 0 9994
2 62138 97.4384 230.0835 0000408 49.1316 310.9954 15.19688613 8393Epoch: 2025-01-24T04:01Z
Definitive object data (Epoch: 2025-01-24T04:01:16.577Z)
| Latitude | -0.00004° |
| Longitude | 46.02983° |
| Altitude | 509.686 km |
| Speed | 7.609 km/s |
| True Right ascension | 15h 20m 20s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -49.09891° |
| Longitude | -142.15997° |
| Altitude | 526.082 km |
| Speed | 7.598 km/s |
| Apparent Right ascension | 03h 18m 19s |
| Apparent Declination | -44° 44' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:46:44 |
| Azimuth | 134.95° SE |
| Elevation | -82.87° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.029 km |
| Perigee altitude | 503.468 km |
| Semi-major axis | 6,881.886 km |
| Eccentricity | 0.0000408 |
| Inclination | 97.4384° |
| RAAN | 230.0835° |
| Arg. of periapsis | 49.1316° |
| True anomaly | 310.99187° |
| Mean anomaly | 310.9954° |
| Eccentric anomaly | 310.99364° |
| Mean motion | 3.80174 °/min |
| BSTAR | 0.0013144 |
| Orbital period | 94.69 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-01-25 02:42:33.434Z | 359.935° N | 2025-01-25 02:45:33.434Z | 262.624° W | 39.253° | 2025-01-25 02:48:33.434Z | 207.233° SW |
| 5 mins | 2025-01-25 13:21:33.434Z | 136.408° SSE | 2025-01-25 13:23:33.434Z | 51.087° ENE | 36.849° | 2025-01-25 13:26:33.434Z | 359.364° N |
Authenticating...
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