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LEMUR 2 SIERRINI, 60579

Orbit data source: Space-Track

LEMUR 2 SIERRINI, 60579 is an American payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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Identifier
60579, 2024-149DR
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
2024-08-16 (2 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, 0.5 m
Radar Cross Section
0.063 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 LEMUR 2 SIERRINI
1 60579U 24149DR  26081.21031412  .00015530  00000-0  98467-3 0  9999
2 60579  97.6861 163.5428 0007023 114.5112 245.6849 15.08992172 87335
Epoch: 2026-03-22T05:02Z
TLE epoch observation values (Epoch: 2026-03-22T05:02:51.139Z)
Latitude
-0.00008°
Longitude
-91.89021°
Altitude
544.349 km
Speed
7.589 km/s
True Right ascension
10h 54m 10s
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
21:59:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.127 km
Perigee altitude
531.415 km
Semi-major axis
6,914.408 km
Eccentricity
0.0007
Inclination
97.6861°
RAAN
163.5428°
Arg. of periapsis
114.5112°
True anomaly
245.61159°
Mean anomaly
245.6849°
Eccentric anomaly
245.64824°
Mean motion
3.77495 °/min
Orbital period
95.37 mins
BSTAR
0.00098467
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