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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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: 5 hours ago
TLE from 5 hours ago
0 FTV 3502
1 369U 62039A 26131.47192898 .00000536 00000-0 56476-4 0 9995
2 369 98.4575 213.1434 0077859 247.1288 112.1695 14.92154971410131Epoch: 2026-05-11T11:19Z
TLE epoch observation values (Epoch: 2026-05-11T11:19:34.663Z)
Latitude
-0.00004°
Longitude
173.9888°
Altitude
615.079 km
Speed
7.54 km/s
True Right ascension
14h 12m 34s
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
00:49:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.508 km
Perigee altitude
534.028 km
Semi-major axis
6,966.405 km
Eccentricity
0.00779
Inclination
98.4575°
RAAN
213.1434°
Arg. of periapsis
247.1288°
True anomaly
112.99269°
Mean anomaly
112.1695°
Eccentric anomaly
112.5814°
Mean motion
3.73276 °/min
Orbital period
96.44 mins
BSTAR
0.000056476
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-11 18:19:49.809Z | 13.781° NNE | 2026-05-11 18:23:49.809Z | 174.927° S | 44.831° | 2026-05-11 18:27:49.809Z | 193.73° SSW |
| 7 mins | 2026-05-12 05:09:49.809Z | 149.792° SSE | 2026-05-12 05:12:49.809Z | 80.029° E | 41.326° | 2026-05-12 05:16:49.809Z | 354.954° N |
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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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 descending order |
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