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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 SQUIRRELCOMM
1 60578U 24149DQ 25286.91119790 .00008920 00000-0 66612-3 0 9999
2 60578 97.6913 4.0025 0006250 163.1061 197.0373 15.03038010 63353Epoch: 2025-10-13T21:52Z
TLE epoch observation values (Epoch: 2025-10-13T21:52:07.498Z)
Latitude
-0.00006°
Longitude
13.26408°
Altitude
564.74 km
Speed
7.577 km/s
True Right ascension
00h 16m 00s
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
10:35:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.869 km
Perigee altitude
550.203 km
Semi-major axis
6,932.673 km
Eccentricity
0.00063
Inclination
97.6913°
RAAN
4.0025°
Arg. of periapsis
163.1061°
True anomaly
197.01633°
Mean anomaly
197.0373°
Eccentric anomaly
197.02681°
Mean motion
3.76004 °/min
Orbital period
95.74 mins
BSTAR
0.00066612
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 17:37:15.313Z | 37.637° NE | 2025-10-14 17:40:15.313Z | 108.577° ESE | 29.756° | 2025-10-14 17:43:15.313Z | 163.06° S |
| 4 mins | 2025-10-15 04:23:15.313Z | 103.196° ESE | 2025-10-15 04:25:15.313Z | 65.252° ENE | 19.08° | 2025-10-15 04:27:15.313Z | 29.408° NE |
| 4 mins | 2025-10-15 05:58:15.313Z | 225.514° WSW | 2025-10-15 06:00:15.313Z | 276.105° WNW | 24.975° | 2025-10-15 06:02:15.313Z | 314.619° NW |
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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