Showing default

LEMUR 2 DELOITTE-1, 63259

Orbit data source: Space-Track

LEMUR 2 DELOITTE-1, 63259 is a payload satellite owned by Spire (US) in SSO that was launched on Sat, 15 Mar 2025 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
63259, 2025-052BB
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2025-03-15 (7 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB  25299.48938924  .00006458  00000-0  59770-3 0  9997
2 63259  97.7120 190.8463 0002024 116.8606 243.2822 14.94856223 33744
Epoch: 2025-10-26T11:44Z
TLE epoch observation values (Epoch: 2025-10-26T11:44:43.230Z)
Latitude
0.00002°
Longitude
-20.43868°
Altitude
586.5 km
Speed
7.567 km/s
True Right ascension
12h 43m 23s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:42:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.24 km
Perigee altitude
578.423 km
Semi-major axis
6,957.969 km
Eccentricity
0.0002
Inclination
97.712°
RAAN
190.8463°
Arg. of periapsis
116.8606°
True anomaly
243.26149°
Mean anomaly
243.2822°
Eccentric anomaly
243.27184°
Mean motion
3.73955 °/min
Orbital period
96.27 mins
BSTAR
0.0005977
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
|