TIGER-6, 58272 (Decayed)
Orbit data source: Space-Track
TIGER-6, 58272 was a payload satellite owned by OQ Tech (RW) in LEO that was launched on Sat, 11 Nov 2023 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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58272 intel report (Beta)
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Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
Space Inventor
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 TIGER-6
1 58272U 23174S 26154.85387241 .04823688 24808-5 85859-3 0 9991
2 58272 97.3593 254.8547 0013670 267.7466 92.2264 16.32402637144280Epoch: 2026-06-03T20:29Z
TLE epoch observation values (Epoch: 2026-06-03T20:29:34.576Z)
Latitude
-0.00004°
Longitude
55.15411°
Altitude
189.694 km
Speed
7.792 km/s
True Right ascension
16h 59m 25s
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
08:28:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
191.875 km
Perigee altitude
173.938 km
Semi-major axis
6,561.044 km
Eccentricity
0.00137
Inclination
97.3593°
RAAN
254.8547°
Arg. of periapsis
267.7466°
True anomaly
92.38292°
Mean anomaly
92.2264°
Eccentric anomaly
92.30466°
Mean motion
4.08398 °/min
Orbital period
88.15 mins
BSTAR
0.00085859
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.TIGER-6 Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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