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: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 26097.71669461 .00011598 00000-0 34797-3 0 9999
2 60471 97.3801 179.6618 0003243 116.8157 243.3418 15.34615040 91359Epoch: 2026-04-07T17:12Z
TLE epoch observation values (Epoch: 2026-04-07T17:12:02.414Z)
Latitude
-0.00002°
Longitude
85.66233°
Altitude
466.171 km
Speed
7.633 km/s
True Right ascension
11h 58m 38s
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
12:54:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.227 km
Perigee altitude
456.792 km
Semi-major axis
6,837.146 km
Eccentricity
0.00032
Inclination
97.3801°
RAAN
179.6618°
Arg. of periapsis
116.8157°
True anomaly
243.30859°
Mean anomaly
243.3418°
Eccentric anomaly
243.3252°
Mean motion
3.83911 °/min
Orbital period
93.77 mins
BSTAR
0.00034797
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-08 18:49:11.913Z | 325.501° NNW | 2026-04-08 18:50:11.913Z | 293.304° NW | 27.971° | 2026-04-08 18:53:11.913Z | 224.609° SW |
| 5 mins | 2026-04-09 05:20:11.913Z | 154.602° SSE | 2026-04-09 05:22:11.913Z | 74.567° E | 42.834° | 2026-04-09 05:25:11.913Z | 354.267° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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