CELTEE 1
NORAD 41850
Payload
LEO
2016-067C
● Active
CONNECTING…
LEO · NORAD 41850
NOW PASSING OVER
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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
506 km
Apogee
507 km
Inclination
98.1°
Period
94.8 min
Mean Motion
15.19701017 rev/day
TLE Epoch
2026-06-19 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude507 km
Orbital Velocity27,407 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.20
Eccentricity0.0001
Semi-Major Axis6,878 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Air Force Research Laboratory (United States)
Launch Date
2016-11-11
Launch Site
Vandenberg SFB, California
Int'l Designator
2016-067C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CELTEE 1 is an active satellite operated by Air Force Research Laboratory (United States), launched on 2016-11-11 from Vandenberg SFB, California. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 506 km and 507 km with an inclination of 98.1°. It travels at approximately 27,407 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.20 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 CELTEE 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
CELTEE 1 orbits at an average altitude of 507 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 CELTEE 1’s average altitude, there are currently 9,552 active payloads and 258 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 54.8% of all active satellites. With an inclination of 98.1°, CELTEE 1 passes over latitudes between 98.1°N and 98.1°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 12,360 active satellites in total, of which 8,922 share a similar altitude band with CELTEE 1.
❓ Frequently Asked Questions
CELTEE 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 507 km altitude. Its 98.1° 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 27,407 km/h.
CELTEE 1 is operated by Air Force Research Laboratory (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41850. You can track CELTEE 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CELTEE 1 was launched on 2016-11-11 from Vandenberg SFB, California, 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks CELTEE 1 (NORAD ID 41850) 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.
CELTEE 1 travels at approximately 27,407 km/h (17,030 mph) — roughly 7.61 km/s. It completes 15.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.