ISIS 1
NORAD 3669
Payload
MEO
1969-009A
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MEO · NORAD 3669
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
577 km
Apogee
3440 km
Inclination
88.4°
Period
127.4 min
Mean Motion
11.30455226 rev/day
TLE Epoch
2026-10-21 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,009 km
Orbital Velocity24,829 km/h
Velocity6.90 km/s
Orbital Period2 hours 7 minutes
Orbits / Day11.30
Eccentricity0.1708
Semi-Major Axis8,380 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇦 CRC (Canada)
Launch Date
1969-01-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1969-009A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ISIS 1 is an active satellite operated by CRC (Canada), launched on 1969-01-30 from Vandenberg Space Force Base, United States on the Isis A launch. After more than 57 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 577 km and 3,440 km with an inclination of 88.4°. It travels at approximately 24,829 km/h (6.90 km/s), completing one full orbit every 2 hours 7 minutes — that’s roughly 11.30 orbits per day. Its orbital eccentricity of 0.1708 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks ISIS 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ISIS 1 orbits at an average altitude of 2,009 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of ISIS 1’s average altitude, there are currently 9 active payloads and 31 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 88.4°, ISIS 1 passes over latitudes between 88.4°N and 88.4°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. Canada operates approximately 75 active satellites in total.
❓ Frequently Asked Questions
ISIS 1 orbits in Medium Earth Orbit (MEO) at altitudes between 577 km (perigee) and 3,440 km (apogee), with an average altitude of approximately 2,009 km. It completes one orbit every 2 hours 7 minutes, travelling at approximately 24,829 km/h (15,428 mph).
ISIS 1 is operated by CRC (Canada). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 3669. You can track ISIS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ISIS 1 was launched on 1969-01-30 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks ISIS 1 (NORAD ID 3669) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
ISIS 1 travels at approximately 24,829 km/h (15,428 mph) — roughly 6.90 km/s. It completes 11.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 sunrises and sunsets every 24 hours.