NANOFF B, 58755
Orbit data source: Space-Track
NANOFF B, 58755 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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58755 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 B
1 58755U 23185S 25305.63157486 .00004301 00000-0 26728-3 0 9990
2 58755 97.5579 11.2444 0013205 14.5808 345.5800 15.10122236 99508Epoch: 2025-11-01T15:09Z
TLE epoch observation values (Epoch: 2025-11-01T15:09:28.067Z)
Latitude
-0.00002°
Longitude
102.71858°
Altitude
530.056 km
Speed
7.603 km/s
True Right ascension
00h 44m 58s
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
10:08:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.938 km
Perigee altitude
523.687 km
Semi-major axis
6,910.949 km
Eccentricity
0.00132
Inclination
97.5579°
RAAN
11.2444°
Arg. of periapsis
14.5808°
True anomaly
345.54226°
Mean anomaly
345.58°
Eccentric anomaly
345.56113°
Mean motion
3.77778 °/min
Orbital period
95.29 mins
BSTAR
0.00026728
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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 B 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 | 2025-11-02 17:10:22.175Z | 22.942° NE | 2025-11-02 17:13:22.175Z | 114.565° SE | 40.931° | 2025-11-02 17:16:22.175Z | 179.643° S |
| 5 mins | 2025-11-03 03:53:22.175Z | 114.328° SE | 2025-11-03 03:55:22.175Z | 66.719° ENE | 24.75° | 2025-11-03 03:58:22.175Z | 12.799° NNE |
| 4 mins | 2025-11-03 05:28:22.175Z | 239.832° WSW | 2025-11-03 05:29:22.175Z | 259.268° W | 17.468° | 2025-11-03 05:32:22.175Z | 311.255° NW |
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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