TIGER-7, 59141
Orbit data source: Space-Track
TIGER-7, 59141 is a payload satellite owned by OQ Tech (RW) in SSO that was launched on Mon, 04 Mar 2024 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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59141 intel report (Beta)
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Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
NanoAvionics
Mission
Operational 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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 TIGER-7
1 59141U 24043AV 26286.40550596 .00014370 00000-0 24626-3 0 9999
2 59141 97.5612 83.0323 0007370 92.8470 267.3625 15.51298299146281Epoch: 2026-10-13T09:43Z
TLE epoch observation values (Epoch: 2026-10-13T09:43:55.714Z)
Latitude
-0.00007°
Longitude
-84.91988°
Altitude
416.297 km
Speed
7.661 km/s
True Right ascension
05h 32m 07s
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
22:01:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
414.868 km
Perigee altitude
404.863 km
Semi-major axis
6,788.002 km
Eccentricity
0.00074
Inclination
97.5612°
RAAN
83.0323°
Arg. of periapsis
92.847°
True anomaly
267.27814°
Mean anomaly
267.3625°
Eccentric anomaly
267.32032°
Mean motion
3.88088 °/min
Orbital period
92.76 mins
BSTAR
0.00024626
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Other satellites on launch #43 in the year 2024 (2024-03-04 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-7 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 | 2026-10-14 10:37:33.077Z | 167.833° S | 2026-10-14 10:40:33.077Z | 329.577° NNW | 82.003° | 2026-10-14 10:43:33.077Z | 347.342° N |
| 4 mins | 2026-10-14 23:27:33.077Z | 14.413° NNE | 2026-10-14 23:29:33.077Z | 183.02° SSW | 66.3° | 2026-10-14 23:31:33.077Z | 191.248° SSW |
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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