LEMUR 1, 40044
Orbit data source: Space-Track
LEMUR 1, 40044 is a payload satellite owned by NanoSatisfi (US) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40044 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NanoSatisfi
Mission
Operational Commercial Technology
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, 1.0 m
Radar Cross Section
0.093 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 1
1 40044U 14033AL 25334.41607152 .00002510 00000-0 30088-3 0 9996
2 40044 97.7601 124.1262 0049612 11.7065 348.5291 14.84083195615977Epoch: 2025-11-30T09:59Z
TLE epoch observation values (Epoch: 2025-11-30T09:59:08.579Z)
Latitude
0.00003°
Longitude
-95.18979°
Altitude
585.487 km
Speed
7.586 km/s
True Right ascension
08h 16m 30s
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
00:29:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
648.181 km
Perigee altitude
578.807 km
Semi-major axis
6,991.631 km
Eccentricity
0.00496
Inclination
97.7601°
RAAN
124.1262°
Arg. of periapsis
11.7065°
True anomaly
348.41535°
Mean anomaly
348.5291°
Eccentric anomaly
348.47229°
Mean motion
3.71258 °/min
Orbital period
96.97 mins
BSTAR
0.00030088
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Other satellites on launch #33 in the year 2014 (2014-06-19 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 1 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 | 2025-12-01 10:23:53.835Z | 185.843° SSW | 2025-12-01 10:25:53.835Z | 244.247° WSW | 41.222° | 2025-12-01 10:29:53.835Z | 339.988° N |
| 5 mins | 2025-12-01 22:10:53.835Z | 56.031° ENE | 2025-12-01 22:12:53.835Z | 92.534° ESE | 22.097° | 2025-12-01 22:15:53.835Z | 142.968° SSE |
| 5 mins | 2025-12-01 23:46:53.835Z | 334.108° NNW | 2025-12-01 23:48:53.835Z | 293.269° NW | 26.178° | 2025-12-01 23:51:53.835Z | 237.541° WSW |
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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