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: 1 day ago
TLE from 1 day ago
0 MEV-1
1 44625U 19067B 26266.94347133 -.00000147 00000-0 00000+0 0 9992
2 44625 0.7977 267.8939 0004270 275.1089 315.6051 1.00272121 62490Epoch: 2026-09-23T22:38Z
TLE epoch observation values (Epoch: 2026-09-23T22:38:35.922Z)
Latitude
-0.63017°
Longitude
156.1176°
Altitude
35,773.141 km
Speed
3.076 km/s
True Right ascension
09h 14m 13s
True Declination
0° 37' 46"
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
00:42:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,805.576 km
Perigee altitude
35,769.566 km
Semi-major axis
42,165.708 km
Eccentricity
0.00043
Inclination
0.7977°
RAAN
267.8939°
Arg. of periapsis
275.1089°
True anomaly
315.57086°
Mean anomaly
315.6051°
Eccentric anomaly
315.58798°
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. |
|---|---|---|---|---|---|---|---|
| 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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