Showing default

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.

Loading next visibility...
Identifier
60578, 2024-149DQ
Orbit
SSO
Country
Flag of USUS
Related 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)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 LEMUR 2 SQUIRRELCOMM
1 60578U 24149DQ  26174.69532460  .00004935  00000-0  33173-3 0  9992
2 60578  97.6714 255.5861 0006008  43.0703 317.0994 15.07214612101380
Epoch: 2026-06-23T16:41Z
TLE epoch observation values (Epoch: 2026-06-23T16:41:16.045Z)
Latitude
0.00001°
Longitude
93.40605°
Altitude
544.735 km
Speed
7.591 km/s
True Right ascension
17h 02m 20s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:15:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.868 km
Perigee altitude
537.553 km
Semi-major axis
6,919.847 km
Eccentricity
0.0006
Inclination
97.6714°
RAAN
255.5861°
Arg. of periapsis
43.0703°
True anomaly
317.05251°
Mean anomaly
317.0994°
Eccentric anomaly
317.07596°
Mean motion
3.7705 °/min
Orbital period
95.48 mins
BSTAR
0.00033173
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|