TANAGER 4001, 60507
Orbit data source: Space-Track
TANAGER 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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 TANAGER 4001
1 60507U 24149AR 25299.24469431 .00000784 00000-0 19343-4 0 9991
2 60507 97.3888 25.5997 0010027 232.5134 127.5203 15.43673530 66942Epoch: 2025-10-26T05:52Z
TLE epoch observation values (Epoch: 2025-10-26T05:52:21.588Z)
Latitude
-0.00001°
Longitude
-97.35392°
Altitude
442.567 km
Speed
7.644 km/s
True Right ascension
01h 42m 23s
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
13:15:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.041 km
Perigee altitude
425.383 km
Semi-major axis
6,810.349 km
Eccentricity
0.001
Inclination
97.3888°
RAAN
25.5997°
Arg. of periapsis
232.5134°
True anomaly
127.61136°
Mean anomaly
127.5203°
Eccentric anomaly
127.56584°
Mean motion
3.86179 °/min
Orbital period
93.22 mins
BSTAR
0.000019343
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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 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 | 2025-10-27 18:13:35.561Z | 42.567° NE | 2025-10-27 18:15:35.561Z | 89.577° E | 25.12° | 2025-10-27 18:18:35.561Z | 158.121° S |
| 4 mins | 2025-10-28 06:14:35.561Z | 196.335° SSW | 2025-10-28 06:16:35.561Z | 277.835° WNW | 35.751° | 2025-10-28 06:18:35.561Z | 330.15° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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