METEOSAT 5 (MOP 2), 21140
Orbit data source: Space-Track
METEOSAT 5 (MOP 2), 21140 is a payload satellite owned by EUMETSAT (ESA) in GEO that was launched on Sat, 02 Mar 1991 UTC via an ARIANE 44LP launch vehicle from the French Guiana (FRGUI). 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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21140 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
Ae/Cannes
Mission
Non-operational Civil Weather
Bus & Motor
METEOSAT, AOCS
Mass
343 kg wet, 284 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Cyl + 1 Ant, 1.7 m
Radar Cross Section
4.680 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 METEOSAT 5 (MOP 2)
1 21140U 91015B 26171.07976014 -.00000050 00000-0 00000-0 0 9991
2 21140 14.6538 349.9765 0009586 266.6298 263.3461 0.98450943130233Epoch: 2026-06-20T01:54Z
TLE epoch observation values (Epoch: 2026-06-20T01:54:51.276Z)
Latitude
2.5503°
Longitude
-136.83145°
Altitude
36,309.034 km
Speed
3.056 km/s
True Right ascension
10h 40m 43s
True Declination
2° 32' 52"
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
23:19:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,346.77 km
Perigee altitude
36,264.936 km
Semi-major axis
42,683.99 km
Eccentricity
0.00096
Inclination
14.6538°
RAAN
349.9765°
Arg. of periapsis
266.6298°
True anomaly
263.23701°
Mean anomaly
263.3461°
Eccentric anomaly
263.29155°
Mean motion
0.24612 °/min
Orbital period
1,462.71 mins
BSTAR
0
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Other satellites on launch #15 in the year 1991 (1991-03-02 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.METEOSAT 5 (MOP 2) 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. |
|---|---|---|---|---|---|---|---|
| 1126 mins | 2026-06-22 12:17:39.852Z | 231.292° WSW | 2026-06-22 21:54:39.852Z | 254.834° W | 28.04° | 2026-06-23 07:03:39.852Z | 236.944° WSW |
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21140 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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