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TDS 1

NORAD 40076 Payload LEO 2014-037H ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
523 km
Apogee
529 km
Inclination
98.4°
Period
95.2 min
Mean Motion
15.13313187 rev/day
TLE Epoch
2026-06-18 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude526 km
Orbital Velocity27,368 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.13
Eccentricity0.0004
Semi-Major Axis6,897 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇬🇧 United Kingdom
Launch Date
2014-07-08
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-037H
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TDS 1 is an active satellite operated by United Kingdom, launched on 2014-07-08 from Baikonur, Kazakhstan. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 523 km and 529 km with an inclination of 98.4°. It travels at approximately 27,368 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.13 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks TDS 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
TDS 1 orbits at an average altitude of 526 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of TDS 1’s average altitude, there are currently 6,799 active payloads and 288 tracked debris or rocket body fragments — notable neighbours include STARLINK-1039, STARLINK-1184, STARLINK-1231. This makes it one of the more crowded altitude bands, containing roughly 39% of all active satellites. With an inclination of 98.4°, TDS 1 passes over latitudes between 98.4°N and 98.4°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. United Kingdom operates approximately 720 active satellites in total, of which 21 share a similar altitude band with TDS 1.
❓ Frequently Asked Questions
TDS 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 526 km altitude. Its 98.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 95 minutes, travelling at 27,368 km/h.
TDS 1 is operated by United Kingdom. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40076. You can track TDS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TDS 1 was launched on 2014-07-08 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks TDS 1 (NORAD ID 40076) 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.
TDS 1 travels at approximately 27,368 km/h (17,006 mph) — roughly 7.60 km/s. It completes 15.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.