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 Civil Weather
Bus & Motor
TIROS I, Unknown motor
Mass
127 kg wet, 127 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.5 m
Radar Cross Section
0.920 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 TIROS 10
1 01430U 65051A 25256.23749333 .00000185 00000-0 69401-4 0 9997
2 01430 98.4773 12.2704 0055282 189.5382 170.4762 14.41453955156013Epoch: 2025-09-13T05:41Z
TLE epoch observation values (Epoch: 2025-09-13T05:41:59.423Z)
Latitude
-0.00006°
Longitude
-65.70092°
Altitude
795.547 km
Speed
7.435 km/s
True Right ascension
00h 49m 04s
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
19:37:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.228 km
Perigee altitude
711.407 km
Semi-major axis
7,128.954 km
Eccentricity
0.00553
Inclination
98.4773°
RAAN
12.2704°
Arg. of periapsis
189.5382°
True anomaly
170.5803°
Mean anomaly
170.4762°
Eccentric anomaly
170.52832°
Mean motion
3.60582 °/min
Orbital period
99.84 mins
BSTAR
0.000069401
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-14 06:49:33.014Z | 121.34° SE | 2025-09-14 06:53:33.014Z | 68.714° E | 24.2° | 2025-09-14 06:57:33.014Z | 13.304° NNE |
| 8 mins | 2025-09-14 08:28:33.014Z | 202.078° SSW | 2025-09-14 08:32:33.014Z | 271.341° WNW | 30.502° | 2025-09-14 08:36:33.014Z | 327.131° NNW |
| 8 mins | 2025-09-14 20:36:33.014Z | 19.141° NNE | 2025-09-14 20:39:33.014Z | 58.154° ENE | 43.09° | 2025-09-14 20:44:33.014Z | 188.161° SSW |
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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