KONDOR FKA 2, 62138
Orbit data source: Space-Track
KONDOR FKA 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). 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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62138 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPOMA?
Mission
Operational Civil Radar Imaging
Bus & Motor
KONDOR, Unknown motor
Mass
1,050 kg wet, 1,050 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Dish, 2.5 m
Radar Cross Section
3.234 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 KONDOR FKA 2
1 62138U 24223A 25252.75105770 .00003894 00000-0 18522-3 0 9996
2 62138 97.4354 95.3151 0001778 86.8332 273.3107 15.19769943 43117Epoch: 2025-09-09T18:01Z
TLE epoch observation values (Epoch: 2025-09-09T18:01:31.385Z)
Latitude
0.00006°
Longitude
-164.10301°
Altitude
509.554 km
Speed
7.609 km/s
True Right ascension
06h 21m 15s
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
22:02:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.726 km
Perigee altitude
502.279 km
Semi-major axis
6,881.64 km
Eccentricity
0.00018
Inclination
97.4354°
RAAN
95.3151°
Arg. of periapsis
86.8332°
True anomaly
273.29036°
Mean anomaly
273.3107°
Eccentric anomaly
273.30053°
Mean motion
3.80194 °/min
Orbital period
94.69 mins
BSTAR
0.00018522
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Other satellites on launch #223 in the year 2024 (2024-11-29 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.KONDOR FKA 2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 13:53:00.154Z | 182.206° SSW | 2025-09-18 13:56:00.154Z | 231.682° WSW | 37.559° | 2025-09-18 14:00:00.154Z | 338.415° N |
| 5 mins | 2025-09-19 02:59:00.154Z | 338.005° N | 2025-09-19 03:01:00.154Z | 279.73° WNW | 29.568° | 2025-09-19 03:04:00.154Z | 222.232° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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