LEMUR 2 EMBRIONOVIS, 56970
Orbit data source: Space-Track
LEMUR 2 EMBRIONOVIS, 56970 is an American payload satellite in SSO that was launched on Mon, 12 Jun 2023 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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56970 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.077 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ 25334.82704735 .00018689 00000-0 59248-3 0 9990
2 56970 97.6028 107.5746 0008817 304.1451 55.8953 15.32725411137257Epoch: 2025-11-30T19:50Z
TLE epoch observation values (Epoch: 2025-11-30T19:50:56.891Z)
Latitude
-0.00007°
Longitude
99.90224°
Altitude
467.405 km
Speed
7.634 km/s
True Right ascension
07h 10m 17s
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
23:29:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.676 km
Perigee altitude
458.609 km
Semi-major axis
6,842.779 km
Eccentricity
0.00088
Inclination
97.6028°
RAAN
107.5746°
Arg. of periapsis
304.1451°
True anomaly
55.97901°
Mean anomaly
55.8953°
Eccentric anomaly
55.93715°
Mean motion
3.83437 °/min
Orbital period
93.89 mins
BSTAR
0.00059248
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Other satellites on launch #84 in the year 2023 (2023-06-12 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 EMBRIONOVIS 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 | 2025-12-01 08:31:37.855Z | 128.705° SE | 2025-12-01 08:33:37.855Z | 83.757° E | 27.19° | 2025-12-01 08:36:37.855Z | 11.909° NNE |
| 5 mins | 2025-12-01 21:29:37.855Z | 37.846° NE | 2025-12-01 21:31:37.855Z | 90.812° ESE | 31.713° | 2025-12-01 21:34:37.855Z | 165.912° S |
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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