PROGRESS MS-29, 62030 (Decayed)
Orbit data source: Space-Track
PROGRESS MS-29, 62030 was a payload satellite owned by RKKE (CIS) in LEO that was launched on Thu, 21 Nov 2024 UTC via a SOYUZ-2-1A 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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62030 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed Civil Spaceship
Bus & Motor
7K-TGM, 11D428A
Mass
7,500 kg wet, 4,325 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Sphere + Cone + 2 Pan, 4.0 m
Radar Cross Section
19.615 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 PROGRESS MS-29
1 62030U 24215A 25182.60262425 .00005250 00000-0 98795-4 0 9994
2 62030 51.6362 235.6237 0002078 320.5297 198.2707 15.50319249 34548Epoch: 2025-07-01T14:27Z
TLE epoch observation values (Epoch: 2025-07-01T14:27:46.735Z)
Latitude
16.50256°
Longitude
-94.70247°
Altitude
417.218 km
Speed
7.663 km/s
True Right ascension
02h 48m 33s
True Declination
16° 24' 16"
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
08:30:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.714 km
Perigee altitude
414.89 km
Semi-major axis
6,794.439 km
Eccentricity
0.00021
Inclination
51.6362°
RAAN
235.6237°
Arg. of periapsis
320.5297°
True anomaly
198.26324°
Mean anomaly
198.2707°
Eccentric anomaly
198.26697°
Mean motion
3.87537 °/min
Orbital period
92.89 mins
BSTAR
0.000098795
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Other satellites on launch #215 in the year 2024 (2024-11-21 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.PROGRESS MS-29 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-26 14:27:58.283Z | 318.562° NNW | 2025-10-26 14:29:58.283Z | 359.737° N | 36.835° | 2025-10-26 14:32:58.283Z | 109.748° ESE |
| 4 mins | 2025-10-27 07:09:58.283Z | 169.201° S | 2025-10-27 07:10:58.283Z | 144.066° SSE | 21.294° | 2025-10-27 07:13:58.283Z | 78.628° E |
| 4 mins | 2025-10-27 08:45:58.283Z | 270.921° WNW | 2025-10-27 08:47:58.283Z | 336.293° NNW | 31.15° | 2025-10-27 08:49:58.283Z | 31.502° NE |
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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