LEMUR 2 ANDIS, 42838
Orbit data source: Space-Track
LEMUR 2 ANDIS, 42838 is a payload satellite owned by Spire (US) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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42838 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.093 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 ANDIS
1 42838U 17042P 25344.05086165 .00028743 00000-0 11167-2 0 9990
2 42838 97.3613 161.3203 0009935 324.1135 35.9435 15.25978884459528Epoch: 2025-12-10T01:13Z
TLE epoch observation values (Epoch: 2025-12-10T01:13:14.446Z)
Latitude
-0.00004°
Longitude
63.98337°
Altitude
485.426 km
Speed
7.626 km/s
True Right ascension
10h 45m 16s
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
14:02:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.622 km
Perigee altitude
477.985 km
Semi-major axis
6,862.941 km
Eccentricity
0.00099
Inclination
97.3613°
RAAN
161.3203°
Arg. of periapsis
324.1135°
True anomaly
36.01039°
Mean anomaly
35.9435°
Eccentric anomaly
35.97694°
Mean motion
3.81749 °/min
Orbital period
94.3 mins
BSTAR
0.0011167
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Other satellites on launch #42 in the year 2017 (2017-07-14 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.LEMUR 2 ANDIS 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 | 2025-12-11 01:24:03.020Z | 336.627° NNW | 2025-12-11 01:26:03.020Z | 279.067° WNW | 28.39° | 2025-12-11 01:29:03.020Z | 222.927° SW |
| 5 mins | 2025-12-11 11:59:03.020Z | 161.657° S | 2025-12-11 12:01:03.020Z | 101.781° ESE | 44.481° | 2025-12-11 12:04:03.020Z | 351.048° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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