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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ 25286.62991340 .00011698 00000-0 38425-3 0 9991
2 56970 97.5995 58.1009 0011386 109.3530 250.8943 15.31671103129872Epoch: 2025-10-13T15:07Z
TLE epoch observation values (Epoch: 2025-10-13T15:07:04.517Z)
Latitude
-0.00003°
Longitude
168.90214°
Altitude
476.488 km
Speed
7.626 km/s
True Right ascension
03h 52m 24s
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
19:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.58 km
Perigee altitude
459.99 km
Semi-major axis
6,845.922 km
Eccentricity
0.00114
Inclination
97.5995°
RAAN
58.1009°
Arg. of periapsis
109.353°
True anomaly
250.77107°
Mean anomaly
250.8943°
Eccentric anomaly
250.83268°
Mean motion
3.83173 °/min
Orbital period
93.95 mins
BSTAR
0.00038425
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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 | 2025-10-14 08:30:03.690Z | 138.722° SSE | 2025-10-14 08:33:03.690Z | 57.748° ENE | 31.259° | 2025-10-14 08:35:03.690Z | 10.794° NNE |
| 6 mins | 2025-10-14 21:28:03.690Z | 25.391° NE | 2025-10-14 21:31:03.690Z | 98.874° ESE | 36.727° | 2025-10-14 21:34:03.690Z | 174.176° 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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