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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Edit Public Description
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
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 TIROS 6
1 397U 62047A 25306.52020505 .00001982 00000-0 19981-3 0 9994
2 397 58.3038 59.5119 0006703 159.7206 200.4109 14.95152360378419Epoch: 2025-11-02T12:29Z
TLE epoch observation values (Epoch: 2025-11-02T12:29:05.716Z)
Latitude
-0.00003°
Longitude
-169.79669°
Altitude
587.686 km
Speed
7.565 km/s
True Right ascension
03h 58m 02s
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
14:36:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.026 km
Perigee altitude
576.696 km
Semi-major axis
6,959.498 km
Eccentricity
0.00067
Inclination
58.3038°
RAAN
59.5119°
Arg. of periapsis
159.7206°
True anomaly
200.38413°
Mean anomaly
200.4109°
Eccentric anomaly
200.39751°
Mean motion
3.73832 °/min
Orbital period
96.3 mins
BSTAR
0.00019981
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-04 09:34:06.605Z | 220.427° SW | 2025-11-04 09:38:06.605Z | 225.403° WSW | 44.964° | 2025-11-04 09:42:06.605Z | 41.586° NE |
| 4 mins | 2025-11-04 11:17:06.605Z | 306.784° NW | 2025-11-04 11:18:06.605Z | 322.968° NNW | 15.768° | 2025-11-04 11:21:06.605Z | 8.526° NNE |
| 5 mins | 2025-11-04 16:21:06.605Z | 356.674° N | 2025-11-04 16:23:06.605Z | 41.057° NE | 25.45° | 2025-11-04 16:26:06.605Z | 94.117° ESE |
| 6 mins | 2025-11-04 18:00:06.605Z | 294.581° NW | 2025-11-04 18:03:06.605Z | 225.198° WSW | 30.995° | 2025-11-04 18:06:06.605Z | 171.528° S |
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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