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: 6 days ago
TLE from 6 days ago
0 COSMOS 2424 (GLONASS)
1 29672U 06062C 25304.38331938 .00000019 00000-0 00000-0 0 9992
2 29672 64.6933 201.9115 0019193 173.4084 186.6775 2.13122506146708Epoch: 2025-10-31T09:11Z
TLE epoch observation values (Epoch: 2025-10-31T09:11:58.794Z)
Latitude
-0.00006°
Longitude
23.98533°
Altitude
19,177.445 km
Speed
3.946 km/s
True Right ascension
13h 27m 38s
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
20:40:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,176.83 km
Perigee altitude
19,078.923 km
Semi-major axis
25,506.014 km
Eccentricity
0.00192
Inclination
64.6933°
RAAN
201.9115°
Arg. of periapsis
173.4084°
True anomaly
186.65199°
Mean anomaly
186.6775°
Eccentric anomaly
186.66474°
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. |
|---|---|---|---|---|---|---|---|
| 284 mins | 2025-11-06 02:05:43.183Z | 314.033° NW | 2025-11-06 04:35:43.183Z | 264.996° W | 44.521° | 2025-11-06 06:49:43.183Z | 188.619° SSW |
| 68 mins | 2025-11-06 12:57:43.183Z | 59.253° ENE | 2025-11-06 13:31:43.183Z | 42.685° NE | 12.979° | 2025-11-06 14:05:43.183Z | 26.692° NE |
| 42 mins | 2025-11-06 23:56:43.183Z | 290.746° WNW | 2025-11-07 00:38:43.183Z | 307.261° NW | 22.339° | 2025-11-07 00:38:43.183Z | 307.261° NW |
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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