LEMUR 2 SQUIRRELCOMM, 60578
Orbit data source: Space-Track
LEMUR 2 SQUIRRELCOMM, 60578 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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60578 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 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 SQUIRRELCOMM
1 60578U 24149DQ 26227.73045008 .00003005 00000-0 20095-3 0 9999
2 60578 97.6684 308.4708 0005127 191.0014 169.1102 15.07727574109374Epoch: 2026-08-15T17:31Z
TLE epoch observation values (Epoch: 2026-08-15T17:31:50.886Z)
Latitude
-0.00009°
Longitude
81.37166°
Altitude
549.697 km
Speed
7.585 km/s
True Right ascension
20h 33m 52s
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
00:21:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.686 km
Perigee altitude
536.592 km
Semi-major axis
6,918.276 km
Eccentricity
0.00051
Inclination
97.6684°
RAAN
308.4708°
Arg. of periapsis
191.0014°
True anomaly
169.12129°
Mean anomaly
169.1102°
Eccentric anomaly
169.11575°
Mean motion
3.77178 °/min
Orbital period
95.45 mins
BSTAR
0.00020095
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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 SQUIRRELCOMM 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-16 17:59:16.576Z | 26.119° NE | 2026-08-16 18:02:16.576Z | 80.998° E | 35.649° | 2026-08-16 18:06:16.576Z | 174.295° S |
| 4 mins | 2026-08-17 04:44:16.576Z | 101.851° ESE | 2026-08-17 04:45:16.576Z | 80.288° E | 21.94° | 2026-08-17 04:48:16.576Z | 20.924° NNE |
| 5 mins | 2026-08-17 06:18:16.576Z | 225.679° WSW | 2026-08-17 06:20:16.576Z | 266.371° W | 20.953° | 2026-08-17 06:23:16.576Z | 317.337° NNW |
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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