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OBJECT CQ

NORAD 101102 Payload LEO 2026-227CQ ● Active
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🛰️ Orbital Parameters
Perigee
508 km
Apogee
512 km
Inclination
97.4°
Period
94.8 min
Mean Motion
15.18577767 rev/day
TLE Epoch
2026-11-03 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude510 km
Orbital Velocity27,400 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.19
Eccentricity0.0003
Semi-Major Axis6,881 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
AMSAT-EA / Hydra Space (Unknown)
Launch Date
2026-10-01
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-227CQ
Object Type
Payload
RCS Size
Small (<0.1 m²)
📖 About This Object
OBJECT CQ is an active satellite operated by AMSAT-EA / Hydra Space (Unknown), launched on 2026-10-01 from Vandenberg Space Force Base, United States on the Transporter-18 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as HADES-L, attributed to AMSAT-EA / Hydra Space. It orbits in Low Earth Orbit (LEO) at altitudes between 508 km and 512 km with an inclination of 97.4°. It travels at approximately 27,400 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.19 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 OBJECT CQ in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT CQ orbits at an average altitude of 510 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 OBJECT CQ’s average altitude, there are currently 10,886 active payloads and 268 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 55.4% of all active satellites. With an inclination of 97.4°, OBJECT CQ passes over latitudes between 97.4°N and 97.4°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.
❓ Frequently Asked Questions
OBJECT CQ is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 510 km altitude. Its 97.4° 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 27,400 km/h.
OBJECT CQ is operated by AMSAT-EA / Hydra Space (Unknown). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 101102. You can track OBJECT CQ in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OBJECT CQ was launched on 2026-10-01 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT CQ (NORAD ID 101102) 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.
OBJECT CQ travels at approximately 27,400 km/h (17,025 mph) — roughly 7.61 km/s. It completes 15.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.