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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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 26112.92222324 .00010992 00000-0 31460-3 0 9990
2 56970 97.6216 255.0881 0010007 146.4958 213.6920 15.36084000159199Epoch: 2026-04-22T22:08Z
TLE epoch observation values (Epoch: 2026-04-22T22:08:00.087Z)
Latitude
-0.00006°
Longitude
72.11104°
Altitude
466.503 km
Speed
7.63 km/s
True Right ascension
17h 00m 21s
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
15:27:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.494 km
Perigee altitude
447.819 km
Semi-major axis
6,832.793 km
Eccentricity
0.001
Inclination
97.6216°
RAAN
255.0881°
Arg. of periapsis
146.4958°
True anomaly
213.62845°
Mean anomaly
213.692°
Eccentric anomaly
213.66022°
Mean motion
3.84278 °/min
Orbital period
93.68 mins
BSTAR
0.0003146
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-23 09:12:15.140Z | 150.223° SSE | 2026-04-23 09:15:15.140Z | 79.898° E | 37.953° | 2026-04-23 09:18:15.140Z | 359.879° N |
| 5 mins | 2026-04-23 22:09:15.140Z | 24.038° NE | 2026-04-23 22:11:15.140Z | 74.151° E | 40.14° | 2026-04-23 22:14:15.140Z | 180.092° SSW |
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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