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: 6 hours ago
TLE from 6 hours ago
0 ENMAP
1 52159U 22033C 26264.97219186 -.00000172 00000-0 -18090-4 0 9999
2 52159 97.9768 345.8295 0001634 85.9441 274.1955 14.74987877240923Epoch: 2026-09-21T23:19Z
TLE epoch observation values (Epoch: 2026-09-21T23:19:57.376Z)
Latitude
-0.00001°
Longitude
-5.00392°
Altitude
648.118 km
Speed
7.534 km/s
True Right ascension
23h 03m 19s
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
21:56:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
643.388 km
Perigee altitude
641.094 km
Semi-major axis
7,020.378 km
Eccentricity
0.00016
Inclination
97.9768°
RAAN
345.8295°
Arg. of periapsis
85.9441°
True anomaly
274.17683°
Mean anomaly
274.1955°
Eccentric anomaly
274.18616°
Mean motion
3.6898 °/min
Orbital period
97.57 mins
BSTAR
-0.00001809
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-22 05:57:20.604Z | 189.655° SSW | 2026-09-22 06:01:20.604Z | 261.769° W | 43.861° | 2026-09-22 06:05:20.604Z | 332.705° NNW |
| 6 mins | 2026-09-22 17:50:20.604Z | 44.027° NE | 2026-09-22 17:52:20.604Z | 86.057° E | 36.264° | 2026-09-22 17:56:20.604Z | 162.9° S |
| 4 mins | 2026-09-22 19:27:20.604Z | 322.737° NNW | 2026-09-22 19:29:20.604Z | 288.014° WNW | 20.005° | 2026-09-22 19:31:20.604Z | 256.491° W |
| 5 mins | 2026-09-23 04:47:20.604Z | 118.974° SE | 2026-09-23 04:50:20.604Z | 57.689° ENE | 29.512° | 2026-09-23 04:52:20.604Z | 21.172° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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