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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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: 10 hours ago
TLE from 10 hours ago
0 FTV 3502
1 00369U 62039A 26104.24594165 .00000768 00000-0 78021-4 0 9990
2 00369 98.4583 183.9232 0078554 337.0545 22.7169 14.92093273406075Epoch: 2026-04-14T05:54Z
TLE epoch observation values (Epoch: 2026-04-14T05:54:09.358Z)
Latitude
-0.00004°
Longitude
-107.04074°
Altitude
543.983 km
Speed
7.618 km/s
True Right ascension
12h 15m 41s
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
22:14:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
643.185 km
Perigee altitude
533.735 km
Semi-major axis
6,966.597 km
Eccentricity
0.00786
Inclination
98.4583°
RAAN
183.9232°
Arg. of periapsis
337.0545°
True anomaly
23.0677°
Mean anomaly
22.7169°
Eccentric anomaly
22.89198°
Mean motion
3.73261 °/min
Orbital period
96.45 mins
BSTAR
0.000078021
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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 | 2026-04-14 17:43:40.981Z | 27.066° NE | 2026-04-14 17:47:40.981Z | 92.862° ESE | 34.774° | 2026-04-14 17:51:40.981Z | 170.561° S |
| 4 mins | 2026-04-14 19:21:40.981Z | 315.913° NNW | 2026-04-14 19:22:40.981Z | 299.605° NW | 16.708° | 2026-04-14 19:25:40.981Z | 255.521° W |
| 5 mins | 2026-04-15 04:35:40.981Z | 110.256° ESE | 2026-04-15 04:37:40.981Z | 61.532° ENE | 25.753° | 2026-04-15 04:40:40.981Z | 10.912° NNE |
| 4 mins | 2026-04-15 06:11:40.981Z | 240.782° WSW | 2026-04-15 06:12:40.981Z | 260.437° W | 18.743° | 2026-04-15 06:15:40.981Z | 310.948° NW |
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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