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: 12 hours ago
TLE from 12 hours ago
0 TIROS 10
1 01430U 65051A 25310.31057182 .00000273 00000-0 96192-4 0 9996
2 01430 98.4839 65.9470 0055902 29.4141 331.0175 14.41501427163801Epoch: 2025-11-06T07:27Z
TLE epoch observation values (Epoch: 2025-11-06T07:27:13.405Z)
Latitude
0.00004°
Longitude
-91.62958°
Altitude
721.664 km
Speed
7.513 km/s
True Right ascension
04h 23m 47s
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
15:39:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.512 km
Perigee altitude
710.81 km
Semi-major axis
7,128.798 km
Eccentricity
0.00559
Inclination
98.4839°
RAAN
65.947°
Arg. of periapsis
29.4141°
True anomaly
330.7052°
Mean anomaly
331.0175°
Eccentric anomaly
330.86154°
Mean motion
3.60594 °/min
Orbital period
99.84 mins
BSTAR
0.000096192
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-06 19:42:57.161Z | 51.983° ENE | 2025-11-06 19:45:57.161Z | 94.918° ESE | 20.517° | 2025-11-06 19:48:57.161Z | 137.049° SSE |
| 7 mins | 2025-11-06 21:21:57.161Z | 347.212° N | 2025-11-06 21:24:57.161Z | 283.935° WNW | 33.543° | 2025-11-06 21:28:57.161Z | 222.945° SW |
| 6 mins | 2025-11-07 06:55:57.161Z | 111.032° ESE | 2025-11-07 06:58:57.161Z | 58.488° ENE | 23.657° | 2025-11-07 07:01:57.161Z | 15.461° NNE |
| 6 mins | 2025-11-07 08:34:57.161Z | 218.643° SW | 2025-11-07 08:36:57.161Z | 257.693° W | 27.418° | 2025-11-07 08:40:57.161Z | 322.742° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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