LEMUR-2 HCS-BAZUS, 67388
Orbit data source: Space-Track
LEMUR-2 HCS-BAZUS, 67388 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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67388 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, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR-2 HCS-BAZUS
1 67388U 26004AB 26093.46353128 .00004027 00000-0 42907-3 0 9994
2 67388 97.8030 93.4375 0002317 15.3627 344.7661 14.89448808 12186Epoch: 2026-04-03T11:07Z
TLE epoch observation values (Epoch: 2026-04-03T11:07:29.102Z)
Latitude
0.00004°
Longitude
94.76894°
Altitude
601.134 km
Speed
7.56 km/s
True Right ascension
06h 13m 44s
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
03:51:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.297 km
Perigee altitude
595.064 km
Semi-major axis
6,974.818 km
Eccentricity
0.00023
Inclination
97.803°
RAAN
93.4375°
Arg. of periapsis
15.3627°
True anomaly
344.75912°
Mean anomaly
344.7661°
Eccentric anomaly
344.76261°
Mean motion
3.72601 °/min
Orbital period
96.62 mins
BSTAR
0.00042907
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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 HCS-BAZUS 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 | 2026-04-04 00:09:18.614Z | 179.806° S | 2026-04-04 00:12:18.614Z | 280.139° WNW | 42.118° | 2026-04-04 00:15:18.614Z | 339.376° N |
| 4 mins | 2026-04-04 11:55:18.614Z | 71.557° E | 2026-04-04 11:56:18.614Z | 90.379° ESE | 18.803° | 2026-04-04 11:59:18.614Z | 139.119° SSE |
| 5 mins | 2026-04-04 13:30:18.614Z | 334.323° NNW | 2026-04-04 13:32:18.614Z | 287.189° WNW | 27.709° | 2026-04-04 13:35:18.614Z | 231.452° 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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