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: 5 hours ago
TLE from 5 hours ago
0 TIROS 6
1 397U 62047A 26036.11988288 .00002095 00000-0 20767-3 0 9991
2 397 58.3030 54.5929 0009279 35.9541 324.2130 14.95609053392560Epoch: 2026-02-05T02:52Z
TLE epoch observation values (Epoch: 2026-02-05T02:52:37.880Z)
Latitude
-0.00001°
Longitude
-123.84162°
Altitude
576.661 km
Speed
7.576 km/s
True Right ascension
03h 38m 22s
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
10:23:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.4 km
Perigee altitude
573.487 km
Semi-major axis
6,958.081 km
Eccentricity
0.00093
Inclination
58.303°
RAAN
54.5929°
Arg. of periapsis
35.9541°
True anomaly
324.15076°
Mean anomaly
324.213°
Eccentric anomaly
324.18189°
Mean motion
3.73946 °/min
Orbital period
96.27 mins
BSTAR
0.00020767
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Other satellites on launch #47 in the year 1962 (1962-09-18 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-05 09:46:53.864Z | 1.307° NNE | 2026-02-05 09:48:53.864Z | 34.089° NE | 16.245° | 2026-02-05 09:50:53.864Z | 65.127° ENE |
| 7 mins | 2026-02-05 11:25:53.864Z | 317.268° NNW | 2026-02-05 11:28:53.864Z | 268.836° W | 44.893° | 2026-02-05 11:32:53.864Z | 141.283° SSE |
| 6 mins | 2026-02-06 03:06:53.864Z | 205.227° SW | 2026-02-06 03:08:53.864Z | 148.148° SSE | 42.647° | 2026-02-06 03:12:53.864Z | 47.013° ENE |
| 4 mins | 2026-02-06 04:47:53.864Z | 303.126° NW | 2026-02-06 04:48:53.864Z | 321.24° NNW | 18.229° | 2026-02-06 04:51:53.864Z | 10.126° NNE |
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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