TIROS 10, 1430
Orbit data source: Space-Track
TIROS 10, 1430 is a payload satellite owned by ESSA (US) in SSO that was launched on Fri, 02 Jul 1965 UTC via a THOR DELTA C 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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1430 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 I, 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: 13 hours ago
TLE from 13 hours ago
0 TIROS 10
1 01430U 65051A 25287.26563283 .00000338 00000-0 11569-3 0 9993
2 01430 98.4812 43.0647 0056544 97.4400 263.3219 14.41484601160482Epoch: 2025-10-14T06:22Z
TLE epoch observation values (Epoch: 2025-10-14T06:22:30.676Z)
Latitude
0°
Longitude
-75.61965°
Altitude
761.464 km
Speed
7.471 km/s
True Right ascension
02h 52m 15s
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
13:39:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.026 km
Perigee altitude
710.407 km
Semi-major axis
7,128.853 km
Eccentricity
0.00565
Inclination
98.4812°
RAAN
43.0647°
Arg. of periapsis
97.44°
True anomaly
262.67889°
Mean anomaly
263.3219°
Eccentric anomaly
263.00034°
Mean motion
3.6059 °/min
Orbital period
99.84 mins
BSTAR
0.00011569
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Other satellites on launch #51 in the year 1965 (1965-07-02 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 10 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-14 20:16:22.090Z | 26.327° NE | 2025-10-14 20:21:22.090Z | 118.558° SE | 35.087° | 2025-10-14 20:25:22.090Z | 172.666° S |
| 5 mins | 2025-10-14 21:57:22.090Z | 324.286° NNW | 2025-10-14 21:59:22.090Z | 293.872° NW | 18.045° | 2025-10-14 22:02:22.090Z | 253.659° W |
| 7 mins | 2025-10-15 07:30:22.090Z | 144.548° SSE | 2025-10-15 07:33:22.090Z | 66.601° ENE | 40.495° | 2025-10-15 07:37:22.090Z | 356.462° 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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