TANAGER-1 4001, 60507
Orbit data source: Space-Track
TANAGER-1 4001, 60507 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 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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60507 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational Commercial Earth Obs Sci
Bus & Motor
TANAGER, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.955 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 TANAGER-1 4001
1 60507U 24149AR 26133.24479593 .00009182 00000-0 19939-3 0 9990
2 60507 97.3208 227.3790 0006069 73.0961 287.0952 15.44572197 97640Epoch: 2026-05-13T05:52Z
TLE epoch observation values (Epoch: 2026-05-13T05:52:30.368Z)
Latitude
-0.00008°
Longitude
-91.75512°
Altitude
434.548 km
Speed
7.652 km/s
True Right ascension
15h 09m 30s
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
05:06:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.696 km
Perigee altitude
425.433 km
Semi-major axis
6,807.702 km
Eccentricity
0.00061
Inclination
97.3208°
RAAN
227.379°
Arg. of periapsis
73.0961°
True anomaly
287.02871°
Mean anomaly
287.0952°
Eccentric anomaly
287.06196°
Mean motion
3.86405 °/min
Orbital period
93.17 mins
BSTAR
0.00019939
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.TANAGER-1 4001 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 | 2026-05-14 06:53:42.957Z | 219.483° SW | 2026-05-14 06:55:42.957Z | 278.124° WNW | 23.579° | 2026-05-14 06:57:42.957Z | 319.515° NNW |
| 4 mins | 2026-05-14 19:45:42.957Z | 326.981° NNW | 2026-05-14 19:46:42.957Z | 301.193° NW | 22.674° | 2026-05-14 19:49:42.957Z | 232.113° WSW |
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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