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
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: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 26046.17912083 .00010677 00000-0 33587-3 0 9997
2 60471 97.3889 128.1339 0000946 4.2493 355.8758 15.33136035 83453Epoch: 2026-02-15T04:17Z
TLE epoch observation values (Epoch: 2026-02-15T04:17:56.039Z)
Latitude
0.00005°
Longitude
-81.54114°
Altitude
468.925 km
Speed
7.632 km/s
True Right ascension
08h 32m 32s
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
16:19:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.057 km
Perigee altitude
462.763 km
Semi-major axis
6,841.547 km
Eccentricity
0.00009
Inclination
97.3889°
RAAN
128.1339°
Arg. of periapsis
4.2493°
True anomaly
355.87502°
Mean anomaly
355.8758°
Eccentric anomaly
355.87541°
Mean motion
3.83541 °/min
Orbital period
93.86 mins
BSTAR
0.00033587
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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 | 2026-02-15 18:58:04.889Z | 326.841° NNW | 2026-02-15 19:00:04.889Z | 277.53° WNW | 20.899° | 2026-02-15 19:02:04.889Z | 239.453° WSW |
| 5 mins | 2026-02-16 05:30:04.889Z | 174.321° S | 2026-02-16 05:32:04.889Z | 244.16° WSW | 44.23° | 2026-02-16 05:35:04.889Z | 344.389° 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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