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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Edit Public Description
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: 13 hours ago
TLE from 13 hours ago
0 PTD-4
1 60565U 24149DB 25289.20665284 .00018448 00000-0 11205-2 0 9997
2 60565 97.7163 9.2846 0004464 157.8353 202.3070 15.10536832 63845Epoch: 2025-10-16T04:57Z
TLE epoch observation values (Epoch: 2025-10-16T04:57:34.805Z)
Latitude
-0.00001°
Longitude
-90.08012°
Altitude
540.486 km
Speed
7.591 km/s
True Right ascension
00h 37m 08s
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
12:35:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.638 km
Perigee altitude
528.469 km
Semi-major axis
6,909.691 km
Eccentricity
0.00045
Inclination
97.7163°
RAAN
9.2846°
Arg. of periapsis
157.8353°
True anomaly
202.28759°
Mean anomaly
202.307°
Eccentric anomaly
202.2973°
Mean motion
3.77881 °/min
Orbital period
95.27 mins
BSTAR
0.0011205
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-16 18:14:12.076Z | 16.098° NNE | 2025-10-16 18:18:12.076Z | 159.569° S | 41.978° | 2025-10-16 18:21:12.076Z | 187.626° SSW |
| 5 mins | 2025-10-17 04:57:12.076Z | 127.543° SE | 2025-10-17 04:59:12.076Z | 83.394° E | 29.038° | 2025-10-17 05:02:12.076Z | 12.59° NNE |
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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