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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 ENMAP
1 52159U 22033C 25349.99995520 .00000833 00000-0 13151-3 0 9991
2 52159 97.9797 69.8664 0001333 82.6846 277.4515 14.74952645199653Epoch: 2025-12-15T23:59Z
TLE epoch observation values (Epoch: 2025-12-15T23:59:56.129Z)
Latitude
0.00005°
Longitude
-15.00793°
Altitude
648.192 km
Speed
7.534 km/s
True Right ascension
04h 39m 27s
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
05:21:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
643.289 km
Perigee altitude
641.417 km
Semi-major axis
7,020.49 km
Eccentricity
0.00013
Inclination
97.9797°
RAAN
69.8664°
Arg. of periapsis
82.6846°
True anomaly
277.43635°
Mean anomaly
277.4515°
Eccentric anomaly
277.44393°
Mean motion
3.68971 °/min
Orbital period
97.57 mins
BSTAR
0.00013151
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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 | 2025-12-16 18:29:02.765Z | 9.139° NNE | 2025-12-16 18:32:02.765Z | 328.99° NNW | 44.091° | 2025-12-16 18:36:02.765Z | 198.493° SSW |
| 7 mins | 2025-12-17 05:26:02.765Z | 161.888° S | 2025-12-17 05:29:02.765Z | 128.136° SE | 44.166° | 2025-12-17 05:33:02.765Z | 349.854° N |
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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