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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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: 4 hours ago
TLE from 4 hours ago
0 MINXSS-2
1 43758U 18099A 26127.81964544 .00027408 00000-0 59487-3 0 9990
2 43758 97.4545 203.0056 0007974 61.7396 298.4656 15.44320558407893Epoch: 2026-05-07T19:40Z
TLE epoch observation values (Epoch: 2026-05-07T19:40:17.366Z)
Latitude
-0°
Longitude
42.27293°
Altitude
433.911 km
Speed
7.653 km/s
True Right ascension
13h 32m 01s
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
08:09:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.74 km
Perigee altitude
424.882 km
Semi-major axis
6,808.448 km
Eccentricity
0.0008
Inclination
97.4545°
RAAN
203.0056°
Arg. of periapsis
61.7396°
True anomaly
298.38523°
Mean anomaly
298.4656°
Eccentric anomaly
298.42542°
Mean motion
3.86341 °/min
Orbital period
93.18 mins
BSTAR
0.00059487
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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 | 2026-05-08 05:07:49.222Z | 173.823° S | 2026-05-08 05:10:49.222Z | 310.653° NW | 41.98° | 2026-05-08 05:12:49.222Z | 342.206° N |
| 4 mins | 2026-05-08 18:00:49.222Z | 1.838° NNE | 2026-05-08 18:02:49.222Z | 251.052° W | 42.199° | 2026-05-08 18:04:49.222Z | 203.221° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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