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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60471 intel report (Beta)
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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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 26084.47824651 .00010857 00000-0 33019-3 0 9995
2 60471 97.3818 166.4195 0002722 143.9853 216.1574 15.34204683 89328Epoch: 2026-03-25T11:28Z
TLE epoch observation values (Epoch: 2026-03-25T11:28:40.498Z)
Latitude
0.00001°
Longitude
171.30978°
Altitude
467.898 km
Speed
7.631 km/s
True Right ascension
11h 05m 40s
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
23:17:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.091 km
Perigee altitude
458.368 km
Semi-major axis
6,838.367 km
Eccentricity
0.00027
Inclination
97.3818°
RAAN
166.4195°
Arg. of periapsis
143.9853°
True anomaly
216.139°
Mean anomaly
216.1574°
Eccentric anomaly
216.1482°
Mean motion
3.83809 °/min
Orbital period
93.8 mins
BSTAR
0.00033019
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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 | 2026-03-25 18:17:59.603Z | 10.682° NNE | 2026-03-25 18:20:59.603Z | 209.272° SW | 44.064° | 2026-03-25 18:23:59.603Z | 194.434° SSW |
| 4 mins | 2026-03-26 04:50:59.603Z | 116.655° SE | 2026-03-26 04:52:59.603Z | 64.56° ENE | 24.117° | 2026-03-26 04:54:59.603Z | 20.329° NNE |
| 4 mins | 2026-03-26 17:47:59.603Z | 45.969° ENE | 2026-03-26 17:49:59.603Z | 104.926° ESE | 28.237° | 2026-03-26 17:51:59.603Z | 154.656° SSE |
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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