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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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: 4 days ago
TLE from 4 days ago
0 COSMOS 2424 (GLONASS)
1 29672U 06062C 26301.14726986 .00000055 00000-0 00000-0 0 9995
2 29672 64.6955 189.8816 0019323 175.4463 184.6595 2.13122736154412Epoch: 2026-10-28T03:32Z
TLE epoch observation values (Epoch: 2026-10-28T03:32:04.115Z)
Latitude
0.00003°
Longitude
100.36366°
Altitude
19,177.926 km
Speed
3.946 km/s
True Right ascension
12h 39m 31s
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
06:01:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,177.144 km
Perigee altitude
19,078.573 km
Semi-major axis
25,505.995 km
Eccentricity
0.00193
Inclination
64.6955°
RAAN
189.8816°
Arg. of periapsis
175.4463°
True anomaly
184.64156°
Mean anomaly
184.6595°
Eccentric anomaly
184.65052°
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. |
|---|---|---|---|---|---|---|---|
| 375 mins | 2026-11-01 19:50:50.407Z | 233.841° WSW | 2026-11-01 23:01:50.407Z | 3.025° NNE | 57.465° | 2026-11-02 02:05:50.407Z | 128.061° SE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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