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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 25338.68206948 .00023973 00000-0 80047-3 0 9998
2 60471 97.3998 55.7560 0001679 169.2373 190.8904 15.31033793 72350Epoch: 2025-12-04T16:22Z
TLE epoch observation values (Epoch: 2025-12-04T16:22:10.803Z)
Latitude
-0.00003°
Longitude
96.47598°
Altitude
476.962 km
Speed
7.627 km/s
True Right ascension
03h 43m 01s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:20:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.827 km
Perigee altitude
468.528 km
Semi-major axis
6,847.815 km
Eccentricity
0.00017
Inclination
97.3998°
RAAN
55.756°
Arg. of periapsis
169.2373°
True anomaly
190.88677°
Mean anomaly
190.8904°
Eccentric anomaly
190.88858°
Mean motion
3.83014 °/min
Orbital period
93.99 mins
BSTAR
0.00080047
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR 2 TOMATOKECHUP 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-05 18:01:31.008Z | 18.599° NNE | 2025-12-05 18:04:31.008Z | 94.361° ESE | 42.53° | 2025-12-05 18:07:31.008Z | 183.134° SSW |
| 4 mins | 2025-12-06 04:36:31.008Z | 102.578° ESE | 2025-12-06 04:37:31.008Z | 80.466° E | 19.637° | 2025-12-06 04:40:31.008Z | 20.428° NNE |
| 4 mins | 2025-12-06 06:09:31.008Z | 231.799° WSW | 2025-12-06 06:11:31.008Z | 276.827° WNW | 18.349° | 2025-12-06 06:13:31.008Z | 312.373° NW |
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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