NANOFF A, 58810
Orbit data source: Space-Track
NANOFF A, 58810 is a payload satellite owned by TUB (DE) in SSO that was launched on Fri, 01 Dec 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58810 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
TUB
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2.7 kg wet, 2.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.046 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NANOFF A
1 58810U 23185T 26263.58497961 .00001933 00000-0 11371-3 0 9991
2 58810 97.5171 329.6729 0009463 348.7694 11.3325 15.12807241147463Epoch: 2026-09-20T14:02Z
TLE epoch observation values (Epoch: 2026-09-20T14:02:22.238Z)
Latitude
0.00006°
Longitude
119.60318°
Altitude
524.312 km
Speed
7.605 km/s
True Right ascension
21h 58m 41s
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
18:03:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.156 km
Perigee altitude
518.092 km
Semi-major axis
6,902.761 km
Eccentricity
0.00095
Inclination
97.5171°
RAAN
329.6729°
Arg. of periapsis
348.7694°
True anomaly
11.35383°
Mean anomaly
11.3325°
Eccentric anomaly
11.34316°
Mean motion
3.7845 °/min
Orbital period
95.12 mins
BSTAR
0.00011371
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Other satellites on launch #185 in the year 2023 (2023-12-01 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.NANOFF A 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 | 2026-09-21 04:26:45.264Z | 161.356° S | 2026-09-21 04:30:45.264Z | 16.661° NNE | 63.452° | 2026-09-21 04:33:45.264Z | 351.651° N |
| 6 mins | 2026-09-21 17:35:45.264Z | 1.538° NNE | 2026-09-21 17:38:45.264Z | 251.572° W | 58.674° | 2026-09-21 17:41:45.264Z | 204.753° SW |
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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