TIROS 3, 162
Orbit data source: Space-Track
TIROS 3, 162 is a payload satellite owned by GSFC (US) in LEO that was launched on Wed, 12 Jul 1961 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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162 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
129 kg wet, 129 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 3
1 00162U 61017A 25312.22998413 .00000203 00000-0 10306-3 0 9993
2 00162 47.8993 293.8955 0043223 120.6008 239.9159 14.45267617359810Epoch: 2025-11-08T05:31Z
TLE epoch observation values (Epoch: 2025-11-08T05:31:10.628Z)
Latitude
-0.00001°
Longitude
163.43863°
Altitude
756.981 km
Speed
7.469 km/s
True Right ascension
19h 35m 34s
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
08:18:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
773.006 km
Perigee altitude
711.453 km
Semi-major axis
7,120.366 km
Eccentricity
0.00432
Inclination
47.8993°
RAAN
293.8955°
Arg. of periapsis
120.6008°
True anomaly
239.48848°
Mean anomaly
239.9159°
Eccentric anomaly
239.70208°
Mean motion
3.61235 °/min
Orbital period
99.66 mins
BSTAR
0.00010306
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Other satellites on launch #17 in the year 1961 (1961-07-12 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 3 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 | 2025-11-10 00:49:12.062Z | 200.64° SSW | 2025-11-10 00:53:12.062Z | 138.724° SSE | 30.76° | 2025-11-10 00:57:12.062Z | 76.552° E |
| 8 mins | 2025-11-10 02:34:12.062Z | 261.013° W | 2025-11-10 02:37:12.062Z | 321.376° NNW | 40.971° | 2025-11-10 02:42:12.062Z | 56.055° ENE |
| 7 mins | 2025-11-10 04:19:12.062Z | 300.077° NW | 2025-11-10 04:22:12.062Z | 349.04° N | 28.815° | 2025-11-10 04:26:12.062Z | 55.613° ENE |
| 8 mins | 2025-11-10 06:04:12.062Z | 311.302° NW | 2025-11-10 06:07:12.062Z | 0.683° NNE | 34.092° | 2025-11-10 06:12:12.062Z | 88.244° E |
| 7 mins | 2025-11-10 07:49:12.062Z | 289.729° WNW | 2025-11-10 07:52:12.062Z | 217.188° SW | 41.644° | 2025-11-10 07:56:12.062Z | 137.673° SSE |
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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