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CALSPHERE 4(A)

NORAD 1520 Payload LEO 1965-065H ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1072 km
Apogee
1175 km
Inclination
89.9°
Period
107.8 min
Mean Motion
13.36291232 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,124 km
Orbital Velocity26,254 km/h
Velocity7.29 km/s
Orbital Period108 minutes
Orbits / Day13.36
Eccentricity0.0069
Semi-Major Axis7,495 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-08-13
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-065H
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CALSPHERE 4(A) is an active satellite operated by United States, launched on 1965-08-13 from Vandenberg Space Force Base, United States on the Dodecapole 2 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 1,072 km and 1,175 km with an inclination of 89.9°. It travels at approximately 26,254 km/h (7.29 km/s), completing one full orbit every 108 minutes — that’s roughly 13.36 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks CALSPHERE 4(A) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CALSPHERE 4(A) orbits at an average altitude of 1,124 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CALSPHERE 4(A)’s average altitude, there are currently 283 active payloads and 451 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041, ONEWEB-0250, ONEWEB-0685. With an inclination of 89.9°, CALSPHERE 4(A) passes over latitudes between 89.9°N and 89.9°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,206 active satellites in total, of which 35 share a similar altitude band with CALSPHERE 4(A).
❓ Frequently Asked Questions
CALSPHERE 4(A) orbits in Low Earth Orbit (LEO) at altitudes between 1,072 km (perigee) and 1,175 km (apogee), with an average altitude of approximately 1,124 km. It completes one orbit every 108 minutes, travelling at approximately 26,254 km/h (16,314 mph).
CALSPHERE 4(A) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1520. You can track CALSPHERE 4(A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CALSPHERE 4(A) was launched on 1965-08-13 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks CALSPHERE 4(A) (NORAD ID 1520) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
CALSPHERE 4(A) travels at approximately 26,254 km/h (16,314 mph) — roughly 7.29 km/s. It completes 13.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.