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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 1
1 40044U 14033AL 26251.21951890 .00001727 00000-0 20219-3 0 9998
2 40044 97.7992 39.2511 0048428 164.0900 196.1850 14.85501481657795Epoch: 2026-09-08T05:16Z
TLE epoch observation values (Epoch: 2026-09-08T05:16:06.432Z)
Latitude
-0.00004°
Longitude
-27.06476°
Altitude
647.574 km
Speed
7.516 km/s
True Right ascension
02h 37m 00s
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
06:13:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.879 km
Perigee altitude
575.204 km
Semi-major axis
6,987.178 km
Eccentricity
0.00484
Inclination
97.7992°
RAAN
39.2511°
Arg. of periapsis
164.09°
True anomaly
196.03121°
Mean anomaly
196.185°
Eccentric anomaly
196.10802°
Mean motion
3.71613 °/min
Orbital period
96.88 mins
BSTAR
0.00020219
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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 | 2026-09-08 22:01:14.776Z | 46.001° ENE | 2026-09-08 22:04:14.776Z | 98.223° ESE | 22.698° | 2026-09-08 22:07:14.776Z | 146.935° SSE |
| 5 mins | 2026-09-08 23:38:14.776Z | 328.895° NNW | 2026-09-08 23:40:14.776Z | 284.746° WNW | 26.259° | 2026-09-08 23:43:14.776Z | 235.105° WSW |
| 4 mins | 2026-09-09 08:55:14.776Z | 95.25° ESE | 2026-09-09 08:57:14.776Z | 62.178° ENE | 18.069° | 2026-09-09 08:59:14.776Z | 31.326° NE |
| 6 mins | 2026-09-09 10:30:14.776Z | 204.132° SW | 2026-09-09 10:32:14.776Z | 247.029° WSW | 39.1° | 2026-09-09 10:36:14.776Z | 329.232° NNW |
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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