Showing default

LEMUR-2-VUKASIN, 66785

Orbit data source: Space-Track

LEMUR-2-VUKASIN, 66785 is an American payload satellite in SSO that was launched on Fri, 28 Nov 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
66785, 2025-276EA
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2025-11-28 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 LEMUR-2-VUKASIN
1 66785U 25276EA  26092.44237509  .00009880  00000-0  81017-3 0  9992
2 66785  97.5295 165.8597 0009127  36.2131 323.9709 14.99405837 18795
Epoch: 2026-04-02T10:37Z
TLE epoch observation values (Epoch: 2026-04-02T10:37:01.207Z)
Latitude
-0.00003°
Longitude
175.81388°
Altitude
566.663 km
Speed
7.581 km/s
True Right ascension
11h 03m 26s
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
08:05:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.067 km
Perigee altitude
559.392 km
Semi-major axis
6,943.867 km
Eccentricity
0.00091
Inclination
97.5295°
RAAN
165.8597°
Arg. of periapsis
36.2131°
True anomaly
323.90933°
Mean anomaly
323.9709°
Eccentric anomaly
323.94012°
Mean motion
3.75095 °/min
Orbital period
95.98 mins
BSTAR
0.00081017
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
|