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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 FIKRETDENGIZ
1 67363U 26004A 26206.45258068 .00004044 00000-0 43989-3 0 9999
2 67363 97.8033 204.4319 0009321 25.7917 334.3763 14.88580419 28979Epoch: 2026-07-25T10:51Z
TLE epoch observation values (Epoch: 2026-07-25T10:51:42.970Z)
Latitude
-0.00003°
Longitude
98.33821°
Altitude
599.539 km
Speed
7.563 km/s
True Right ascension
13h 37m 43s
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
11:56:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.899 km
Perigee altitude
592.891 km
Semi-major axis
6,977.532 km
Eccentricity
0.00093
Inclination
97.8033°
RAAN
204.4319°
Arg. of periapsis
25.7917°
True anomaly
334.33006°
Mean anomaly
334.3763°
Eccentric anomaly
334.35318°
Mean motion
3.72383 °/min
Orbital period
96.67 mins
BSTAR
0.00043989
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-25 23:52:58.524Z | 164.313° S | 2026-07-25 23:56:58.524Z | 47.953° ENE | 44.847° | 2026-07-26 00:00:58.524Z | 348.908° N |
| 6 mins | 2026-07-26 13:14:58.524Z | 350.746° N | 2026-07-26 13:17:58.524Z | 269.889° W | 34.4° | 2026-07-26 13:20:58.524Z | 218.041° SW |
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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