VOLGA R/B, 44425 (Decayed)
Orbit data source: Space-Track
VOLGA R/B, 44425 was space debris in LEO originally from a launch on Wed, 10 Jul 2019 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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44425 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
VOLGA, Unknown motor
Mass
~1,120 kg wet, 1,120 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.6 m
Radar Cross Section
6.585 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 VOLGA R/B
1 44425U 19039E 25195.10029677 .18814549 26529-5 11945-3 0 9997
2 44425 97.4315 321.7118 0014193 257.5828 276.4005 16.53639047336604Epoch: 2025-07-14T02:24Z
TLE epoch observation values (Epoch: 2025-07-14T02:24:25.64Z)
Latitude
6.03828°
Longitude
174.17694°
Altitude
131.438 km
Speed
7.828 km/s
True Right ascension
09h 29m 59s
True Declination
5° 59' 56"
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
23:29:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
135.794 km
Perigee altitude
117.33 km
Semi-major axis
6,504.699 km
Eccentricity
0.00142
Inclination
97.4315°
RAAN
321.7118°
Arg. of periapsis
257.5828°
True anomaly
276.23884°
Mean anomaly
276.4005°
Eccentric anomaly
276.31967°
Mean motion
4.13716 °/min
Orbital period
87.02 mins
BSTAR
0.00011945
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Other satellites on launch #39 in the year 2019 (2019-07-10 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.VOLGA R/B Visibility
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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. |
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| This satellite is decayed. |
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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