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, 0.1 m
Radar Cross Section
0.054 m²
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 FIKRETDENGIZ
1 67363U 26004A 26146.55193532 .00004321 00000-0 47479-3 0 9993
2 67363 97.8013 145.4463 0007958 200.1715 159.9189 14.88140787 20065Epoch: 2026-05-26T13:14Z
TLE epoch observation values (Epoch: 2026-05-26T13:14:47.211Z)
Latitude
0.00003°
Longitude
62.62584°
Altitude
612 km
Speed
7.55 km/s
True Right ascension
09h 41m 47s
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
04:33:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.324 km
Perigee altitude
595.217 km
Semi-major axis
6,978.907 km
Eccentricity
0.0008
Inclination
97.8013°
RAAN
145.4463°
Arg. of periapsis
200.1715°
True anomaly
159.95018°
Mean anomaly
159.9189°
Eccentric anomaly
159.93454°
Mean motion
3.72273 °/min
Orbital period
96.7 mins
BSTAR
0.00047479
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-26 23:04:08.566Z | 120.076° SE | 2026-05-26 23:07:08.566Z | 73.6° E | 21.626° | 2026-05-26 23:10:08.566Z | 21.245° NNE |
| 5 mins | 2026-05-27 00:41:08.566Z | 223.062° SW | 2026-05-27 00:43:08.566Z | 266.949° W | 25.139° | 2026-05-27 00:46:08.566Z | 319.284° NNW |
| 6 mins | 2026-05-27 12:25:08.566Z | 30.68° NE | 2026-05-27 12:28:08.566Z | 100.431° ESE | 35.896° | 2026-05-27 12:31:08.566Z | 168.201° S |
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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