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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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
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TIROS 10
1 01430U 65051A 26275.55193172 .00000080 00000-0 37632-4 0 9993
2 01430 98.5159 34.4799 0056306 116.3038 244.3951 14.41661198211389Epoch: 2026-10-02T13:14Z
TLE epoch observation values (Epoch: 2026-10-02T13:14:46.900Z)
Latitude
0.00005°
Longitude
-175.48777°
Altitude
773.505 km
Speed
7.458 km/s
True Right ascension
02h 17m 55s
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
16:06:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.272 km
Perigee altitude
709.999 km
Semi-major axis
7,128.272 km
Eccentricity
0.00563
Inclination
98.5159°
RAAN
34.4799°
Arg. of periapsis
116.3038°
True anomaly
243.81502°
Mean anomaly
244.3951°
Eccentric anomaly
244.10488°
Mean motion
3.60634 °/min
Orbital period
99.82 mins
BSTAR
0.000037632
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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 | 2026-10-03 07:41:16.613Z | 149.836° SSE | 2026-10-03 07:45:16.613Z | 91.474° ESE | 57.301° | 2026-10-03 07:50:16.613Z | 355.186° N |
| 4 mins | 2026-10-03 09:23:16.613Z | 249.498° W | 2026-10-03 09:24:16.613Z | 262.721° W | 14.666° | 2026-10-03 09:27:16.613Z | 300.839° NW |
| 4 mins | 2026-10-03 19:51:16.613Z | 70.081° E | 2026-10-03 19:53:16.613Z | 101.001° ESE | 17.994° | 2026-10-03 19:55:16.613Z | 128.488° SE |
| 8 mins | 2026-10-03 21:28:16.613Z | 355.103° N | 2026-10-03 21:31:16.613Z | 305.748° NW | 43.675° | 2026-10-03 21:36:16.613Z | 217.31° SW |
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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