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LEMUR 2 TOMATOKECHUP, 60471

Orbit data source: Space-Track

LEMUR 2 TOMATOKECHUP, 60471 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
60471, 2024-149D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D   26002.17023322  .00020281  00000-0  66059-3 0  9990
2 60471  97.3961  84.1807 0003048 103.9002 256.2579 15.31866463 76713
Epoch: 2026-01-02T04:05Z
TLE epoch observation values (Epoch: 2026-01-02T04:05:08.150Z)
Latitude
0.00002°
Longitude
-78.91756°
Altitude
473.847 km
Speed
7.629 km/s
True Right ascension
05h 36m 43s
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
12:27:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.28 km
Perigee altitude
465.107 km
Semi-major axis
6,845.33 km
Eccentricity
0.0003
Inclination
97.3961°
RAAN
84.1807°
Arg. of periapsis
103.9002°
True anomaly
256.22398°
Mean anomaly
256.2579°
Eccentric anomaly
256.24094°
Mean motion
3.83223 °/min
Orbital period
93.94 mins
BSTAR
0.00066059
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