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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 TANAGER-1 4001
1 60507U 24149AR 26178.26452616 .00000378 00000-0 99165-5 0 9997
2 60507 97.2406 272.4919 0002944 269.9285 90.1627 15.44777616104594Epoch: 2026-06-27T06:20Z
TLE epoch observation values (Epoch: 2026-06-27T06:20:55.060Z)
Latitude
0.00003°
Longitude
-98.11869°
Altitude
435.166 km
Speed
7.651 km/s
True Right ascension
18h 09m 58s
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
12:43:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.961 km
Perigee altitude
426.953 km
Semi-major axis
6,807.094 km
Eccentricity
0.00029
Inclination
97.2406°
RAAN
272.4919°
Arg. of periapsis
269.9285°
True anomaly
90.19644°
Mean anomaly
90.1627°
Eccentric anomaly
90.17957°
Mean motion
3.86456 °/min
Orbital period
93.15 mins
BSTAR
0.0000099165
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-28 05:48:09.628Z | 132.086° SE | 2026-06-28 05:51:09.628Z | 64.506° ENE | 24.728° | 2026-06-28 05:53:09.628Z | 18.451° NNE |
| 4 mins | 2026-06-28 18:41:09.628Z | 50.164° ENE | 2026-06-28 18:43:09.628Z | 112.404° ESE | 25.873° | 2026-06-28 18:45:09.628Z | 156.026° SSE |
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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