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: 15 hours ago
TLE from 15 hours ago
0 TIROS 10
1 01430U 65051A 25340.15743624 .00000406 00000-0 13642-3 0 9990
2 01430 98.4858 95.5948 0054326 299.2310 60.3453 14.41524342168105Epoch: 2025-12-06T03:46Z
TLE epoch observation values (Epoch: 2025-12-06T03:46:42.491Z)
Latitude
0.00001°
Longitude
-36.27145°
Altitude
737.404 km
Speed
7.496 km/s
True Right ascension
06h 22m 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
16:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
789.313 km
Perigee altitude
711.858 km
Semi-major axis
7,128.723 km
Eccentricity
0.00543
Inclination
98.4858°
RAAN
95.5948°
Arg. of periapsis
299.231°
True anomaly
60.88811°
Mean anomaly
60.3453°
Eccentric anomaly
60.61652°
Mean motion
3.606 °/min
Orbital period
99.83 mins
BSTAR
0.00013642
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Other satellites on launch #51 in the year 1965 (1965-07-02 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 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-06 19:23:42.668Z | 65.334° ENE | 2025-12-06 19:25:42.668Z | 89.575° E | 13.711° | 2025-12-06 19:27:42.668Z | 114.188° SE |
| 8 mins | 2025-12-06 21:01:42.668Z | 3.137° NNE | 2025-12-06 21:04:42.668Z | 304.796° NW | 42.36° | 2025-12-06 21:09:42.668Z | 205.581° SW |
| 5 mins | 2025-12-07 06:36:42.668Z | 89.182° E | 2025-12-07 06:38:42.668Z | 60.381° ENE | 17.477° | 2025-12-07 06:41:42.668Z | 22.828° NE |
| 8 mins | 2025-12-07 08:13:42.668Z | 190.325° SSW | 2025-12-07 08:16:42.668Z | 254.97° W | 38.749° | 2025-12-07 08:21:42.668Z | 336.925° NNW |
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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