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: 1 day ago
TLE from 1 day ago
0 FTV 3502
1 00369U 62039A 25301.61898840 .00002423 00000-0 23540-3 0 9991
2 00369 98.4833 3.8802 0080814 161.0031 199.4231 14.91271798381087Epoch: 2025-10-28T14:51Z
TLE epoch observation values (Epoch: 2025-10-28T14:51:20.597Z)
Latitude
0.00002°
Longitude
103.84049°
Altitude
650.187 km
Speed
7.504 km/s
True Right ascension
00h 15m 31s
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
10:13:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.342 km
Perigee altitude
534.701 km
Semi-major axis
6,969.159 km
Eccentricity
0.00808
Inclination
98.4833°
RAAN
3.8802°
Arg. of periapsis
161.0031°
True anomaly
199.11806°
Mean anomaly
199.4231°
Eccentric anomaly
199.27029°
Mean motion
3.73055 °/min
Orbital period
96.5 mins
BSTAR
0.0002354
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 17:11:43.399Z | 14.536° NNE | 2025-10-29 17:14:43.399Z | 121.246° SE | 44.94° | 2025-10-29 17:17:43.399Z | 192.756° SSW |
| 7 mins | 2025-10-30 04:01:43.399Z | 150.163° SSE | 2025-10-30 04:04:43.399Z | 77.168° E | 41.349° | 2025-10-30 04:08:43.399Z | 354.497° 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 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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