Skip to content
Home Library Satellite Directory VELA 9/10 INTERSTAGE

VELA 9/10 INTERSTAGE

NORAD 60001 Payload HEO 1969-046G ● Active
CONNECTING… HEO · NORAD 60001
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
7670 km
Apogee
120993 km
Inclination
17.6°
Period
3118.7 min
Mean Motion
0.46172440 rev/day
TLE Epoch
2026-08-15 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude64,332 km
Orbital Velocity8,548 km/h
Velocity2.37 km/s
Orbital Period52.0 hours
Orbits / Day0.46
Eccentricity0.8014
Semi-Major Axis70,703 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1969-05-23
Launch Site
Cape Canaveral, Florida
Int'l Designator
1969-046G
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
VELA 9/10 INTERSTAGE is an active satellite operated by United States, launched on 1969-05-23 from Cape Canaveral, Florida on the ERS 29 launch. After more than 57 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 7,670 km and 120,993 km with an inclination of 17.6°. It travels at approximately 8,548 km/h (2.37 km/s), completing one full orbit every 52.0 hours — that’s roughly 0.46 orbits per day. Its orbital eccentricity of 0.8014 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks VELA 9/10 INTERSTAGE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
VELA 9/10 INTERSTAGE follows a Highly Elliptical Orbit, sweeping between 7,670 km (perigee) and 120,993 km (apogee). It spends most of its 52.0 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 17.6°, VELA 9/10 INTERSTAGE passes over latitudes between 17.6°N and 17.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,723 active satellites in total.
❓ Frequently Asked Questions
VELA 9/10 INTERSTAGE follows a Highly Elliptical Orbit, swinging between 7,670 km (perigee) and 120,993 km (apogee). It spends most of its 52.0 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
VELA 9/10 INTERSTAGE is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60001. You can track VELA 9/10 INTERSTAGE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
VELA 9/10 INTERSTAGE was launched on 1969-05-23 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks VELA 9/10 INTERSTAGE (NORAD ID 60001) 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.
VELA 9/10 INTERSTAGE’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 8,548 km/h (2.37 km/s), completing one revolution every 52.0 hours. Learn more about highly elliptical orbits.