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LEMUR-2 WOBLER, 67368

Orbit data source: Space-Track

LEMUR-2 WOBLER, 67368 is a payload satellite owned by Spire/Lux (US) in SSO that was launched on Sun, 11 Jan 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
67368, 2026-004F
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
2026-01-11 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 LEMUR-2 WOBLER
1 67368U 26004F   26206.42334600  .00004142  00000-0  44845-3 0  9999
2 67368  97.8058 204.5275 0008614  20.3861 339.7698 14.88759994 28989
Epoch: 2026-07-25T10:09Z
TLE epoch observation values (Epoch: 2026-07-25T10:09:37.094Z)
Latitude
-0.00004°
Longitude
108.98711°
Altitude
599.203 km
Speed
7.563 km/s
True Right ascension
13h 38m 06s
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
11:11:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.844 km
Perigee altitude
592.824 km
Semi-major axis
6,976.971 km
Eccentricity
0.00086
Inclination
97.8058°
RAAN
204.5275°
Arg. of periapsis
20.3861°
True anomaly
339.73563°
Mean anomaly
339.7698°
Eccentric anomaly
339.75272°
Mean motion
3.72428 °/min
Orbital period
96.66 mins
BSTAR
0.00044845
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