FTV 3502, 369
Orbit data source: Space-Track
FTV 3502, 369 is a payload satellite owned by SAFSP (US) in SSO that was launched on Thu, 23 Aug 1962 UTC via an SCOUT X-2M 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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369 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
P35, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 FTV 3502
1 00369U 62039A 25316.24592441 .00005162 00000-0 49198-3 0 9994
2 00369 98.4810 19.5992 0081336 113.9568 247.0192 14.91364489383265Epoch: 2025-11-12T05:54Z
TLE epoch observation values (Epoch: 2025-11-12T05:54:07.869Z)
Latitude
-0.00006°
Longitude
-120.55446°
Altitude
619.232 km
Speed
7.537 km/s
True Right ascension
01h 18m 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
10:36:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.414 km
Perigee altitude
534.05 km
Semi-major axis
6,968.869 km
Eccentricity
0.00813
Inclination
98.481°
RAAN
19.5992°
Arg. of periapsis
113.9568°
True anomaly
246.16455°
Mean anomaly
247.0192°
Eccentric anomaly
246.59153°
Mean motion
3.73078 °/min
Orbital period
96.49 mins
BSTAR
0.00049198
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Other satellites on launch #39 in the year 1962 (1962-08-23 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.FTV 3502 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 | 2025-11-12 17:45:30.253Z | 340.291° N | 2025-11-12 17:47:30.253Z | 272.243° WNW | 32.914° | 2025-11-12 17:50:30.253Z | 218.897° SW |
| 7 mins | 2025-11-13 04:33:30.253Z | 177.068° S | 2025-11-13 04:37:30.253Z | 266.747° W | 41.325° | 2025-11-13 04:40:30.253Z | 336.798° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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