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: 8 hours ago
TLE from 8 hours ago
0 KONDOR FKA 2
1 62138U 24223A 25298.84162649 .00006844 00000-0 32338-3 0 9993
2 62138 97.4330 140.7205 0001820 87.9282 272.2161 15.19727183 50116Epoch: 2025-10-25T20:11Z
TLE epoch observation values (Epoch: 2025-10-25T20:11:56.528Z)
Latitude
-0.00007°
Longitude
163.26859°
Altitude
509.705 km
Speed
7.609 km/s
True Right ascension
09h 22m 52s
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
23:11:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.884 km
Perigee altitude
502.379 km
Semi-major axis
6,881.769 km
Eccentricity
0.00018
Inclination
97.433°
RAAN
140.7205°
Arg. of periapsis
87.9282°
True anomaly
272.19526°
Mean anomaly
272.2161°
Eccentric anomaly
272.20568°
Mean motion
3.80183 °/min
Orbital period
94.69 mins
BSTAR
0.00032338
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Other satellites on launch #223 in the year 2024 (2024-11-29 UTC)
No other RSOs were in this launch
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-26 13:42:37.648Z | 172.767° S | 2025-10-26 13:45:37.648Z | 297.209° NW | 43.87° | 2025-10-26 13:48:37.648Z | 344.499° N |
| 5 mins | 2025-10-27 02:47:37.648Z | 352.807° N | 2025-10-27 02:49:37.648Z | 302.186° NW | 36.193° | 2025-10-27 02:52:37.648Z | 215.126° 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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