ENMAP, 52159
Orbit data source: Space-Track
ENMAP, 52159 is a payload satellite owned by DLR (DE) in SSO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52159 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
KTHR/OHB
Mission
Operational Civil Imaging
Bus & Motor
ENMAP, AOCS
Mass
916 kg wet, ~857 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.0 m
Radar Cross Section
5.352 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ENMAP
1 52159U 22033C 26150.18826480 .00000706 00000-0 11255-3 0 9993
2 52159 97.9796 232.6930 0001404 88.5224 271.6145 14.74970461224001Epoch: 2026-05-30T04:31Z
TLE epoch observation values (Epoch: 2026-05-30T04:31:06.078Z)
Latitude
-0.00011°
Longitude
-82.79019°
Altitude
648.23 km
Speed
7.534 km/s
True Right ascension
15h 30m 46s
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
01:38:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
643.282 km
Perigee altitude
641.311 km
Semi-major axis
7,020.433 km
Eccentricity
0.00014
Inclination
97.9796°
RAAN
232.693°
Arg. of periapsis
88.5224°
True anomaly
271.59842°
Mean anomaly
271.6145°
Eccentric anomaly
271.60646°
Mean motion
3.68975 °/min
Orbital period
97.57 mins
BSTAR
0.00011255
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Other satellites on launch #33 in the year 2022 (2022-04-01 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.ENMAP 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-30 18:07:14.853Z | 23.986° NE | 2026-05-30 18:10:14.853Z | 76.283° E | 39.706° | 2026-05-30 18:14:14.853Z | 178.243° S |
| 6 mins | 2026-05-31 05:05:14.853Z | 134.6° SE | 2026-05-31 05:07:14.853Z | 91.929° ESE | 35.022° | 2026-05-31 05:11:14.853Z | 2.882° NNE |
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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