COSMOS 2424 (GLONASS), 29672
Orbit data source: Space-Track
COSMOS 2424 (GLONASS), 29672 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Mon, 25 Dec 2006 UTC via a PROTON-K/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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29672 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Non-operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,450 kg wet, ~1,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Arm + 2 Pan, 3.9 m
Radar Cross Section
8.145 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 COSMOS 2424 (GLONASS)
1 29672U 06062C 25276.23039940 .00000002 00000-0 00000-0 0 9994
2 29672 64.6954 202.8475 0019292 174.9208 185.1083 2.13122699146107Epoch: 2025-10-03T05:31Z
TLE epoch observation values (Epoch: 2025-10-03T05:31:46.508Z)
Latitude
0.00003°
Longitude
107.7196°
Altitude
19,177.799 km
Speed
3.946 km/s
True Right ascension
13h 31m 22s
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
11:16:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,177.067 km
Perigee altitude
19,078.655 km
Semi-major axis
25,505.998 km
Eccentricity
0.00193
Inclination
64.6954°
RAAN
202.8475°
Arg. of periapsis
174.9208°
True anomaly
185.08866°
Mean anomaly
185.1083°
Eccentric anomaly
185.09848°
Mean motion
0.53282 °/min
Orbital period
675.65 mins
BSTAR
0
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Other satellites on launch #62 in the year 2006 (2006-12-25 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.COSMOS 2424 (GLONASS) 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. |
|---|---|---|---|---|---|---|---|
| 322 mins | 2025-10-14 01:39:20.762Z | 291.887° WNW | 2025-10-14 04:40:20.762Z | 69.447° E | 44.583° | 2025-10-14 07:01:20.762Z | 168.289° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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