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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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ISO8601 Format

Identifier

56970, 2023-084AQ

Orbit

SSO

Country

US

Related business

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Imaging

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

10 kg wet, 10 kg dry

Launch date (UTC)

2023-06-12 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

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 & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ  26016.62196653  .00005901  00000-0  18379-3 0  9993
2 56970  97.6058 155.7077 0010678 129.5983 230.6203 15.33625592144427

Epoch: 2026-01-16T14:55Z

TLE epoch observation values (Epoch: 2026-01-16T14:55:37.908Z)

Latitude

-0.00005°

Longitude

175.74115°

Altitude

472.751 km

Speed

7.627 km/s

True Right ascension

10h 22m 49s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

05:21:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

469.266 km

Perigee altitude

454.658 km

Semi-major axis

6,840.099 km

Eccentricity

0.00107

Inclination

97.6058°

RAAN

155.7077°

Arg. of periapsis

129.5983°

True anomaly

230.5258°

Mean anomaly

230.6203°

Eccentric anomaly

230.57304°

Mean motion

3.83663 °/min

Orbital period

93.83 mins

BSTAR

0.00018379

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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)

RUNNER-1 (TYVAK-1005), 56953

FOSSASAT2E17 (FEROX), 56935 (Decayed)

BLACKJACK ACES-2, 56955

NUSAT-43 (R DIENG-KUNTZ), 56968

ICEYE-X25, 56963

OBJECT K, 56941 (Decayed)

SPACEBEE-173, 56978 (Decayed)

NUSAT-41 (C PAYNE-G), 56944

MISR-B-2, 56940 (Decayed)

ION SCV-011, 56957

GREGOIRE, 56946

AAC-AIS-SAT2, 56996

ICEYE-X30, 56947

OUTPOST MISSION 1, 56226

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

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.
4 mins	2026-01-17 08:18:13.955Z	109.426° ESE	2026-01-17 08:20:13.955Z	72.901° E	16.42°	2026-01-17 08:22:13.955Z	33.121° NE

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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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Check out LEMUR 2 EMBRIONOVIS, 56970 on other resources

View LEMUR 2 EMBRIONOVIS, 56970 on NASA - NSSDCA Website

View LEMUR 2 EMBRIONOVIS, 56970 on Heavens-Above

View LEMUR 2 EMBRIONOVIS, 56970 on Keep Track

View LEMUR 2 EMBRIONOVIS, 56970 on Celestrak

View LEMUR 2 EMBRIONOVIS, 56970 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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