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 Commercial Com/MetRO
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
Box + 2 Pan, 0.2 m
Radar Cross Section
0.054 m²
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 WOBLER
1 67368U 26004F 26146.26133615 .00004356 00000-0 47631-3 0 9990
2 67368 97.8039 145.2504 0007490 192.1021 168.0017 14.88333287 20030Epoch: 2026-05-26T06:16Z
TLE epoch observation values (Epoch: 2026-05-26T06:16:19.443Z)
Latitude
-0.00001°
Longitude
167.33208°
Altitude
611.295 km
Speed
7.551 km/s
True Right ascension
09h 41m 00s
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
03:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.395 km
Perigee altitude
594.941 km
Semi-major axis
6,978.305 km
Eccentricity
0.00075
Inclination
97.8039°
RAAN
145.2504°
Arg. of periapsis
192.1021°
True anomaly
168.01953°
Mean anomaly
168.0017°
Eccentric anomaly
168.01061°
Mean motion
3.72322 °/min
Orbital period
96.69 mins
BSTAR
0.00047631
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-27 00:09:03.329Z | 180.171° SSW | 2026-05-27 00:12:03.329Z | 267.55° W | 42.15° | 2026-05-27 00:16:03.329Z | 341.246° N |
| 4 mins | 2026-05-27 11:55:03.329Z | 60.597° ENE | 2026-05-27 11:57:03.329Z | 97.314° ESE | 19.34° | 2026-05-27 11:59:03.329Z | 132.125° SE |
| 6 mins | 2026-05-27 13:30:03.329Z | 342.574° N | 2026-05-27 13:33:03.329Z | 279.569° WNW | 26.666° | 2026-05-27 13:36:03.329Z | 230.299° WSW |
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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