PROGRESS MS-34, 68837
Orbit data source: Space-Track
PROGRESS MS-34, 68837 is a payload satellite owned by RKKE (CIS) in LEO that was launched on Sat, 25 Apr 2026 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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68837 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Operational spacecraft
Bus & Motor
7K-TGM, 11D428A
Mass
7,419 kg wet, 4,325 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 PROGRESS MS-34
1 68837U 26093A 26171.15661001 .00008669 00000-0 16345-3 0 9990
2 68837 51.6329 285.3962 0004555 207.7610 152.3136 15.49327998572199Epoch: 2026-06-20T03:45Z
TLE epoch observation values (Epoch: 2026-06-20T03:45:31.104Z)
Latitude
-0.00004°
Longitude
-39.35871°
Altitude
422.173 km
Speed
7.658 km/s
True Right ascension
19h 01m 35s
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
10:19:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.296 km
Perigee altitude
416.103 km
Semi-major axis
6,797.337 km
Eccentricity
0.00046
Inclination
51.6329°
RAAN
285.3962°
Arg. of periapsis
207.761°
True anomaly
152.33784°
Mean anomaly
152.3136°
Eccentric anomaly
152.32572°
Mean motion
3.87289 °/min
Orbital period
92.95 mins
BSTAR
0.00016345
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Other satellites on launch #93 in the year 2026 (2026-04-25 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.PROGRESS MS-34 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 09:20:19.701Z | 173.044° S | 2026-06-21 09:22:19.701Z | 127.064° SE | 19.654° | 2026-06-21 09:24:19.701Z | 86.112° E |
| 4 mins | 2026-06-21 10:57:19.701Z | 273.596° WNW | 2026-06-21 10:58:19.701Z | 306.17° NW | 32.818° | 2026-06-21 11:01:19.701Z | 37.742° NE |
| 4 mins | 2026-06-21 15:50:19.701Z | 344.109° N | 2026-06-21 15:51:19.701Z | 12.055° NNE | 26.048° | 2026-06-21 15:54:19.701Z | 88.474° E |
| 4 mins | 2026-06-21 17:27:19.701Z | 265.598° W | 2026-06-21 17:28:19.701Z | 233.26° WSW | 27.89° | 2026-06-21 17:31:19.701Z | 161.272° S |
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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