TIROS 6, 397
Orbit data source: Space-Track
TIROS 6, 397 is a payload satellite owned by GSFC (US) in LEO that was launched on Tue, 18 Sep 1962 UTC via a THOR DELTA launch vehicle from the Air Force Eastern Test Range (AFETR). 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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397 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS, Unknown motor
Mass
127 kg wet, 127 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 TIROS 6
1 00397U 62047A 26275.90163359 .00000557 00000-0 69344-4 0 9993
2 00397 58.3024 208.7771 0006666 22.7062 337.4280 14.96242347428449Epoch: 2026-10-02T21:38Z
TLE epoch observation values (Epoch: 2026-10-02T21:38:21.142Z)
Latitude
0°
Longitude
-127.42792°
Altitude
575.652 km
Speed
7.576 km/s
True Right ascension
13h 55m 06s
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
22:04:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.617 km
Perigee altitude
573.343 km
Semi-major axis
6,956.117 km
Eccentricity
0.00067
Inclination
58.3024°
RAAN
208.7771°
Arg. of periapsis
22.7062°
True anomaly
337.39866°
Mean anomaly
337.428°
Eccentric anomaly
337.41333°
Mean motion
3.74104 °/min
Orbital period
96.23 mins
BSTAR
0.000069344
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Other satellites on launch #47 in the year 1962 (1962-09-18 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.TIROS 6 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 | 2026-10-03 04:31:56.906Z | 346.729° N | 2026-10-03 04:34:56.906Z | 33.766° NE | 20.581° | 2026-10-03 04:37:56.906Z | 80.746° E |
| 7 mins | 2026-10-03 06:11:56.906Z | 309.314° NW | 2026-10-03 06:14:56.906Z | 235.045° WSW | 63.548° | 2026-10-03 06:18:56.906Z | 151.55° SSE |
| 6 mins | 2026-10-03 21:51:56.906Z | 221.903° SW | 2026-10-03 21:54:56.906Z | 30.774° NE | 76.602° | 2026-10-03 21:57:56.906Z | 40.728° NE |
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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