LEMUR-2 FIKRETDENGIZ, 67363
Orbit data source: Space-Track
LEMUR-2 FIKRETDENGIZ, 67363 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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67363 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, 0.3 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 FIKRETDENGIZ
1 67363U 26004A 26263.98539939 .00001992 00000-0 21795-3 0 9999
2 67363 97.8093 261.1475 0008596 173.7201 186.4125 14.88922382 37530Epoch: 2026-09-20T23:38Z
TLE epoch observation values (Epoch: 2026-09-20T23:38:58.507Z)
Latitude
-0.00005°
Longitude
-93.468°
Altitude
610.301 km
Speed
7.551 km/s
True Right ascension
17h 24m 35s
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
11:33:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.323 km
Perigee altitude
592.329 km
Semi-major axis
6,976.463 km
Eccentricity
0.00086
Inclination
97.8093°
RAAN
261.1475°
Arg. of periapsis
173.7201°
True anomaly
186.40151°
Mean anomaly
186.4125°
Eccentric anomaly
186.407°
Mean motion
3.72469 °/min
Orbital period
96.65 mins
BSTAR
0.00021795
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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 FIKRETDENGIZ 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 | 2026-09-21 23:57:48.705Z | 168.325° S | 2026-09-22 00:01:48.705Z | 334.487° NNW | 71.112° | 2026-09-22 00:04:48.705Z | 346.196° N |
| 5 mins | 2026-09-22 13:19:48.705Z | 342.062° N | 2026-09-22 13:21:48.705Z | 290.902° WNW | 39.579° | 2026-09-22 13:24:48.705Z | 225.093° 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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