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 26171.22919462 .00016922 00000-0 74011-3 0 9990
2 60565 97.6961 260.1861 0002743 55.7599 304.3896 15.22142304101281Epoch: 2026-06-20T05:30Z
TLE epoch observation values (Epoch: 2026-06-20T05:30:02.415Z)
Latitude
-0.00001°
Longitude
-90.77078°
Altitude
501.399 km
Speed
7.614 km/s
True Right ascension
17h 20m 44s
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
07:21:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.241 km
Perigee altitude
494.47 km
Semi-major axis
6,874.493 km
Eccentricity
0.00027
Inclination
97.6961°
RAAN
260.1861°
Arg. of periapsis
55.7599°
True anomaly
304.36366°
Mean anomaly
304.3896°
Eccentric anomaly
304.37663°
Mean motion
3.80787 °/min
Orbital period
94.54 mins
BSTAR
0.00074011
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:18:57.886Z | 118.251° SE | 2026-06-21 05:20:57.886Z | 75.104° E | 23.475° | 2026-06-21 05:23:57.886Z | 15.219° NNE |
| 5 mins | 2026-06-21 18:21:57.886Z | 40.634° NE | 2026-06-21 18:23:57.886Z | 88.569° E | 29.537° | 2026-06-21 18:26:57.886Z | 161.041° S |
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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