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: 2 days ago
TLE from 2 days ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 26258.67369000 .00009467 00000-0 25790-3 0 9994
2 60471 97.3745 341.0336 0000326 207.0199 153.1028 15.37701136116062Epoch: 2026-09-15T16:10Z
TLE epoch observation values (Epoch: 2026-09-15T16:10:06.815Z)
Latitude
-0.00008°
Longitude
103.86896°
Altitude
456.223 km
Speed
7.639 km/s
True Right ascension
22h 44m 08s
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
03:02:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.073 km
Perigee altitude
449.627 km
Semi-major axis
6,827.987 km
Eccentricity
0.00003
Inclination
97.3745°
RAAN
341.0336°
Arg. of periapsis
207.0199°
True anomaly
153.10449°
Mean anomaly
153.1028°
Eccentric anomaly
153.10364°
Mean motion
3.84684 °/min
Orbital period
93.58 mins
BSTAR
0.0002579
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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 | 2026-09-17 18:41:33.667Z | 2.739° NNE | 2026-09-17 18:44:33.667Z | 310.528° NW | 52.179° | 2026-09-17 18:47:33.667Z | 209.123° SW |
| 5 mins | 2026-09-18 05:13:33.667Z | 128.805° SE | 2026-09-18 05:15:33.667Z | 66.156° ENE | 36.287° | 2026-09-18 05:18:33.667Z | 5.408° NNE |
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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