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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Edit Public Description
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, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 TIGER-7
1 59141U 24043AV 26033.83539712 .00013651 00000-0 29229-3 0 9998
2 59141 97.5287 179.3338 0005749 308.5179 51.5553 15.44890280107207Epoch: 2026-02-02T20:02Z
TLE epoch observation values (Epoch: 2026-02-02T20:02:58.311Z)
Latitude
-0.00003°
Longitude
105.56586°
Altitude
432.388 km
Speed
7.654 km/s
True Right ascension
11h 57m 20s
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
15:39:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
432.552 km
Perigee altitude
424.725 km
Semi-major axis
6,806.776 km
Eccentricity
0.00057
Inclination
97.5287°
RAAN
179.3338°
Arg. of periapsis
308.5179°
True anomaly
51.60692°
Mean anomaly
51.5553°
Eccentric anomaly
51.58111°
Mean motion
3.86484 °/min
Orbital period
93.15 mins
BSTAR
0.00029229
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-03 23:03:03.463Z | 326.089° NNW | 2026-02-03 23:04:03.463Z | 296.794° NW | 25.172° | 2026-02-03 23:07:03.463Z | 227.918° WSW |
| 5 mins | 2026-02-04 09:30:03.463Z | 153.288° SSE | 2026-02-04 09:32:03.463Z | 63.457° ENE | 42.186° | 2026-02-04 09:35:03.463Z | 354.2° N |
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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