PTD-R (TYVAK-0127), 60523 (Decayed)
Orbit data source: Space-Track
PTD-R (TYVAK-0127), 60523 was an American payload satellite in LEO 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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60523 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Terran Orbital
Mission
Decayed 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: 1 week ago
TLE from 1 week ago
0 PTD-R (TYVAK-0127)
1 60523U 24149BH 26166.10956565 .08494645 25249-5 54306-3 0 9992
2 60523 97.3587 267.1148 0014665 263.0313 96.9318 16.40205066103118Epoch: 2026-06-15T02:37Z
TLE epoch observation values (Epoch: 2026-06-15T02:37:46.472Z)
Latitude
-0.00007°
Longitude
-35.72949°
Altitude
169.682 km
Speed
7.804 km/s
True Right ascension
17h 48m 27s
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
21:56:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
171.654 km
Perigee altitude
152.471 km
Semi-major axis
6,540.2 km
Eccentricity
0.00147
Inclination
97.3587°
RAAN
267.1148°
Arg. of periapsis
263.0313°
True anomaly
97.09858°
Mean anomaly
96.9318°
Eccentric anomaly
97.0152°
Mean motion
4.10352 °/min
Orbital period
87.73 mins
BSTAR
0.00054306
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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-R (TYVAK-0127) Visibility
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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. |
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| This satellite is decayed. |
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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