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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Edit Public Description
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: 23 hours ago
TLE from 23 hours ago
0 NANOFF A
1 58810U 23185T 25305.63153752 .00004558 00000-0 28311-3 0 9998
2 58810 97.5578 11.2238 0010920 19.4169 340.7474 15.10124480 98679Epoch: 2025-11-01T15:09Z
TLE epoch observation values (Epoch: 2025-11-01T15:09:24.841Z)
Latitude
-0.00006°
Longitude
102.71146°
Altitude
531.764 km
Speed
7.601 km/s
True Right ascension
00h 44m 53s
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
10:08:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.352 km
Perigee altitude
525.259 km
Semi-major axis
6,910.943 km
Eccentricity
0.00109
Inclination
97.5578°
RAAN
11.2238°
Arg. of periapsis
19.4169°
True anomaly
340.70609°
Mean anomaly
340.7474°
Eccentric anomaly
340.72675°
Mean motion
3.77779 °/min
Orbital period
95.29 mins
BSTAR
0.00028311
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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 | 2025-11-02 17:09:23.067Z | 19.575° NNE | 2025-11-02 17:13:23.067Z | 120.175° SE | 40.713° | 2025-11-02 17:16:23.067Z | 179.93° S |
| 5 mins | 2025-11-03 03:53:23.067Z | 113.283° SE | 2025-11-03 03:55:23.067Z | 64.757° ENE | 24.734° | 2025-11-03 03:58:23.067Z | 12.247° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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