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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67368 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 WOBLER
1 67368U 26004F 26095.56365218 .00006183 00000-0 67916-3 0 9990
2 67368 97.8052 95.3290 0008680 23.9021 336.2597 14.87982450 12499Epoch: 2026-04-05T13:31Z
TLE epoch observation values (Epoch: 2026-04-05T13:31:39.548Z)
Latitude
-0.00001°
Longitude
58.54694°
Altitude
601.727 km
Speed
7.562 km/s
True Right ascension
06h 21m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:59:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.324 km
Perigee altitude
595.208 km
Semi-major axis
6,979.403 km
Eccentricity
0.00087
Inclination
97.8052°
RAAN
95.329°
Arg. of periapsis
23.9021°
True anomaly
336.21962°
Mean anomaly
336.2597°
Eccentric anomaly
336.23966°
Mean motion
3.72234 °/min
Orbital period
96.71 mins
BSTAR
0.00067916
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Other satellites on launch #4 in the year 2026 (2026-01-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR-2 WOBLER Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-05 23:20:59.072Z | 130.325° SE | 2026-04-05 23:23:59.072Z | 71.094° E | 29.185° | 2026-04-05 23:26:59.072Z | 11.959° NNE |
| 4 mins | 2026-04-06 00:57:59.072Z | 234.282° WSW | 2026-04-06 00:59:59.072Z | 268.766° W | 17.549° | 2026-04-06 01:01:59.072Z | 301.835° NW |
| 7 mins | 2026-04-06 12:41:59.072Z | 18.782° NNE | 2026-04-06 12:44:59.072Z | 111.301° ESE | 43.795° | 2026-04-06 12:48:59.072Z | 187.128° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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