PTD-4, 60565
Orbit data source: Space-Track
PTD-4, 60565 is an American payload satellite 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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60565 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Terran Orbital
Mission
Operational Civil Technology
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, 1.1 m
Radar Cross Section
0.189 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 PTD-4
1 60565U 24149DB 26080.20273665 .00025690 00000-0 12520-2 0 9993
2 60565 97.6973 167.2881 0002179 5.2079 354.9177 15.18317698 87459Epoch: 2026-03-21T04:51Z
TLE epoch observation values (Epoch: 2026-03-21T04:51:56.446Z)
Latitude
0.00001°
Longitude
-84.42392°
Altitude
512.509 km
Speed
7.608 km/s
True Right ascension
11h 09m 09s
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
01:02:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.406 km
Perigee altitude
506.405 km
Semi-major axis
6,886.042 km
Eccentricity
0.00022
Inclination
97.6973°
RAAN
167.2881°
Arg. of periapsis
5.2079°
True anomaly
354.91549°
Mean anomaly
354.9177°
Eccentric anomaly
354.91659°
Mean motion
3.79829 °/min
Orbital period
94.78 mins
BSTAR
0.001252
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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.PTD-4 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 | 2026-03-22 04:45:02.495Z | 100.537° ESE | 2026-03-22 04:47:02.495Z | 66.331° ENE | 14.745° | 2026-03-22 04:49:02.495Z | 32.526° NE |
| 4 mins | 2026-03-22 06:19:02.495Z | 216.118° SW | 2026-03-22 06:21:02.495Z | 275.961° WNW | 28.083° | 2026-03-22 06:23:02.495Z | 319.262° NNW |
| 4 mins | 2026-03-22 17:50:02.495Z | 59.157° ENE | 2026-03-22 17:52:02.495Z | 100.989° ESE | 19.286° | 2026-03-22 17:54:02.495Z | 138.31° SSE |
| 4 mins | 2026-03-22 19:24:02.495Z | 326.768° NNW | 2026-03-22 19:26:02.495Z | 280.099° WNW | 21.565° | 2026-03-22 19:28:02.495Z | 242.448° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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