MINXSS-2, 43758
Orbit data source: Space-Track
MINXSS-2, 43758 is a payload satellite owned by CU-LASP (US) in SSO that was launched on Mon, 03 Dec 2018 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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43758 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
CU-LASP
Mission
Operational Amateur Astronomy
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3.52 kg wet, 3.52 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Ant, 0.4 m
Radar Cross Section
0.075 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 MINXSS-2
1 43758U 18099A 25319.67672161 .00030558 00000-0 96539-3 0 9996
2 43758 97.4840 26.7078 0009212 317.9391 42.1143 15.32727677381271Epoch: 2025-11-15T16:14Z
TLE epoch observation values (Epoch: 2025-11-15T16:14:28.747Z)
Latitude
0.00002°
Longitude
88.08558°
Altitude
466.107 km
Speed
7.636 km/s
True Right ascension
01h 46m 49s
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
07:20:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.934 km
Perigee altitude
458.327 km
Semi-major axis
6,842.768 km
Eccentricity
0.00092
Inclination
97.484°
RAAN
26.7078°
Arg. of periapsis
317.9391°
True anomaly
42.18515°
Mean anomaly
42.1143°
Eccentric anomaly
42.14972°
Mean motion
3.83438 °/min
Orbital period
93.89 mins
BSTAR
0.00096539
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.MINXSS-2 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-16 17:52:10.003Z | 353.66° N | 2025-11-16 17:55:10.003Z | 267.648° W | 33.162° | 2025-11-16 17:57:10.003Z | 220.856° SW |
| 5 mins | 2025-11-17 04:25:10.003Z | 146.275° SSE | 2025-11-17 04:27:10.003Z | 87.65° E | 38.66° | 2025-11-17 04:30:10.003Z | 359.729° N |
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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