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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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, 0.4 m
Radar Cross Section
0.093 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 LEMUR 2 ANDIS
1 42838U 17042P 26289.78356772 .00026565 00000-0 67534-3 0 9993
2 42838 97.3687 110.9079 0006573 288.9691 71.0842 15.39575511507138Epoch: 2026-10-16T18:48Z
TLE epoch observation values (Epoch: 2026-10-16T18:48:20.251Z)
Latitude
-0.00002°
Longitude
163.5239°
Altitude
449.029 km
Speed
7.644 km/s
True Right ascension
07h 23m 37s
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
18:39:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.786 km
Perigee altitude
439.817 km
Semi-major axis
6,822.439 km
Eccentricity
0.00066
Inclination
97.3687°
RAAN
110.9079°
Arg. of periapsis
288.9691°
True anomaly
71.15547°
Mean anomaly
71.0842°
Eccentric anomaly
71.11983°
Mean motion
3.85153 °/min
Orbital period
93.47 mins
BSTAR
0.00067534
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-17 01:36:58.257Z | 335.501° NNW | 2026-10-17 01:38:58.257Z | 275.125° WNW | 30.61° | 2026-10-17 01:40:58.257Z | 230.231° WSW |
| 4 mins | 2026-10-17 12:06:58.257Z | 147.148° SSE | 2026-10-17 12:07:58.257Z | 116.959° SE | 56.671° | 2026-10-17 12:10:58.257Z | 356.897° N |
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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