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LEMUR 2 MANO, 57390

Orbit data source: Space-Track

LEMUR 2 MANO, 57390 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 18 Jul 2023 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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https://www.satcat.com/sats-embedded/57390?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

57390, 2023-100E

Orbit

SSO

Last TLE update

20 hours ago

Origin

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Com/MetRO

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

5 kg wet, 5 kg dry

Launch date (UTC)

2023-07-18 (2 years ago)

Launch vehicle

ELECTRON

Launch site

Rocket Lab Launch Complex (RLLC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.3 m

Radar Cross Section

0.054 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 20 hours ago

0 LEMUR 2 MANO
1 57390U 23100E   25201.83664083  .00025890  00000-0  81990-3 0  9992
2 57390  99.4539 150.6692 0008680  72.3839 287.8343 15.32716412110737

Epoch: 2025-07-20T20:04Z

TLE epoch observation values (Epoch: 2025-07-20T20:04:45.767Z)

Latitude

-0.00012°

Longitude

-89.37515°

Altitude

468.937 km

Speed

7.633 km/s

True Right ascension

10h 02m 40s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-42.14072°

Longitude

-79.68482°

Altitude

486.01 km

Speed

7.62 km/s

Apparent Right ascension

13h 52m 27s

Apparent Declination

-52° 52' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:13:57

Azimuth

128.103° SE

Elevation

-53.789°

Doppler factor

Orbital elements

Apogee altitude

470.7 km

Perigee altitude

458.821 km

Semi-major axis

6,842.898 km

Eccentricity

0.00087

Inclination

99.4539°

RAAN

150.6692°

Arg. of periapsis

72.3839°

True anomaly

287.73958°

Mean anomaly

287.8343°

Eccentric anomaly

287.78694°

Mean motion

3.83427 °/min

Orbital period

93.89 mins

BSTAR

0.0008199

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Other satellites on launch #100 in the year 2023 (2023-07-18 UTC)

LEMUR 2 DEVERILL-M-T, 57391

LEO 3, 57392

ELECTRON KICK STAGE R/B, 57393

ELECTRON R/B, 57394 (Decayed)

LEMUR 2 MANO Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-21 21:17:41.978Z	229.145° WSW	2025-07-21 21:18:41.978Z	253.489° W	20.955°	2025-07-21 21:21:41.978Z	315.072° NNW
4 mins	2025-07-22 10:14:41.978Z	340.561° N	2025-07-22 10:16:41.978Z	290.161° WNW	25.557°	2025-07-22 10:18:41.978Z	240.49° WSW

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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Authenticating...

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Check out LEMUR 2 MANO, 57390 on other resources

View LEMUR 2 MANO, 57390 on NASA - NSSDCA Website

View LEMUR 2 MANO, 57390 on Heavens-Above

View LEMUR 2 MANO, 57390 on Keep Track

View LEMUR 2 MANO, 57390 on Celestrak

View LEMUR 2 MANO, 57390 on Gunter's Space Page

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