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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NANOFF A
1 58810U 23185T 26092.15066258 .00004468 00000-0 26560-3 0 9997
2 58810 97.5318 160.6775 0009716 202.1660 157.9151 15.11742259121559Epoch: 2026-04-02T03:36Z
TLE epoch observation values (Epoch: 2026-04-02T03:36:57.246Z)
Latitude
-0.0001°
Longitude
-84.06428°
Altitude
540.185 km
Speed
7.589 km/s
True Right ascension
10h 42m 42s
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
20:08:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.579 km
Perigee altitude
521.159 km
Semi-major axis
6,906.006 km
Eccentricity
0.00097
Inclination
97.5318°
RAAN
160.6775°
Arg. of periapsis
202.166°
True anomaly
157.95691°
Mean anomaly
157.9151°
Eccentric anomaly
157.93601°
Mean motion
3.78184 °/min
Orbital period
95.19 mins
BSTAR
0.0002656
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-02 16:53:43.830Z | 33.619° NE | 2026-04-02 16:56:43.830Z | 98.233° ESE | 30.413° | 2026-04-02 16:59:43.830Z | 162.404° S |
| 4 mins | 2026-04-03 03:36:43.830Z | 95.866° ESE | 2026-04-03 03:37:43.830Z | 77.676° E | 16.874° | 2026-04-03 03:40:43.830Z | 25.775° NE |
| 5 mins | 2026-04-03 05:10:43.830Z | 221.501° SW | 2026-04-03 05:12:43.830Z | 275.359° WNW | 26.223° | 2026-04-03 05:15:43.830Z | 325.713° NNW |
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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