MEV-1, 44625
Orbit data source: Space-Track
MEV-1, 44625 is a payload satellite owned by Space Logistics (US) in GEO that was launched on Wed, 09 Oct 2019 UTC via a PROTON-M/BRIZ-M 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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44625 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS SSG
Mission
Operational Commercial Technology
Bus & Motor
GEOSTAR-3, IHI BT-4?
Mass
2,326 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 36.6 m
Radar Cross Section
30.713 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 MEV-1
1 44625U 19067B 26240.62423735 -.00000146 00000-0 00000+0 0 9991
2 44625 0.8646 268.1263 0004205 250.6949 198.8983 1.00271884 62297Epoch: 2026-08-28T14:58Z
TLE epoch observation values (Epoch: 2026-08-28T14:58:54.107Z)
Latitude
0.84567°
Longitude
156.13178°
Altitude
35,802.811 km
Speed
3.073 km/s
True Right ascension
23h 50m 48s
True Declination
0° 50' 41"
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
09:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,805.368 km
Perigee altitude
35,769.907 km
Semi-major axis
42,165.774 km
Eccentricity
0.00042
Inclination
0.8646°
RAAN
268.1263°
Arg. of periapsis
250.6949°
True anomaly
198.8827°
Mean anomaly
198.8983°
Eccentric anomaly
198.8905°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #67 in the year 2019 (2019-10-09 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.MEV-1 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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| MEV-1 is likely not visible in the next few days. |
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44625 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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