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LEMUR-2 IRINA, 68480

Orbit data source: Space-Track

LEMUR-2 IRINA, 68480 is a Luxembourger payload satellite in SSO that was launched on Mon, 30 Mar 2026 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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Identifier
68480, 2026-067BS
Orbit
SSO
Country
Flag of LULU / LUXE
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-03-30 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 LEMUR-2 IRINA
1 68480U 26067BS  26126.84207732  .00003428  00000-0  33783-3 0  9991
2 68480  97.7608  85.8030 0005525  61.9244 298.2534 14.92678057  5560
Epoch: 2026-05-06T20:12Z
TLE epoch observation values (Epoch: 2026-05-06T20:12:35.480Z)
Latitude
0.00005°
Longitude
-82.04161°
Altitude
590.811 km
Speed
7.566 km/s
True Right ascension
05h 43m 12s
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
21:01:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.455 km
Perigee altitude
582.759 km
Semi-major axis
6,964.744 km
Eccentricity
0.00055
Inclination
97.7608°
RAAN
85.803°
Arg. of periapsis
61.9244°
True anomaly
298.19761°
Mean anomaly
298.2534°
Eccentric anomaly
298.22551°
Mean motion
3.7341 °/min
Orbital period
96.41 mins
BSTAR
0.00033783
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Documentation

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