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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 (2 years 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: 1 day ago

TLE from 1 day ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D   26255.68021439  .00008416  00000-0  22993-3 0  9998
2 60471  97.3754 338.0279 0000141 299.1387  60.9843 15.37648150115605
Epoch: 2026-09-12T16:19Z
TLE epoch observation values (Epoch: 2026-09-12T16:19:30.523Z)
Latitude
-0.00008°
Longitude
101.46499°
Altitude
456.134 km
Speed
7.639 km/s
True Right ascension
22h 32m 06s
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
08:59:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.103 km
Perigee altitude
449.911 km
Semi-major axis
6,828.144 km
Eccentricity
0.00001
Inclination
97.3754°
RAAN
338.0279°
Arg. of periapsis
299.1387°
True anomaly
60.98571°
Mean anomaly
60.9843°
Eccentric anomaly
60.98501°
Mean motion
3.84671 °/min
Orbital period
93.59 mins
BSTAR
0.00022993
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