SIRIUS 2 (GE-1E)
NORAD 25049
Payload
GEO
1997-071A
● Active
CONNECTING…
GEO · NORAD 25049
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36016 km
Apogee
36047 km
Inclination
12.0°
Period
1448.6 min
Mean Motion
0.99404717 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,032 km
Orbital Velocity11,038 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0004
Semi-Major Axis42,403 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇸🇪 Sweden
Launch Date
1997-11-11
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-071A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SIRIUS 2 (GE-1E) is an active satellite operated by Sweden, launched on 1997-11-11 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,016 km and 36,047 km with an inclination of 12.0°. It travels at approximately 11,038 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 0.99 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks SIRIUS 2 (GE-1E) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SIRIUS 2 (GE-1E) occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 12.0°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of SIRIUS 2 (GE-1E)’s average altitude, there are currently 74 active payloads and 29 tracked debris or rocket body fragments. Sweden operates approximately 15 active satellites in total.
❓ Frequently Asked Questions
SIRIUS 2 (GE-1E) orbits at approximately 36,032 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,038 km/h — it just keeps pace with the ground below. With an inclination of 12.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SIRIUS 2 (GE-1E) is operated by Sweden. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25049. You can track SIRIUS 2 (GE-1E) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SIRIUS 2 (GE-1E) was launched on 1997-11-11 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks SIRIUS 2 (GE-1E) (NORAD ID 25049) 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.
SIRIUS 2 (GE-1E) travels at approximately 11,038 km/h (6,858 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.