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MOI-1A

NORAD 101107 Payload LEO 2026-227CV ● Active
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🛰️ Orbital Parameters
Perigee
512 km
Apogee
520 km
Inclination
97.4°
Period
95.0 min
Mean Motion
15.16607362 rev/day
TLE Epoch
2026-10-20 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude516 km
Orbital Velocity27,388 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.17
Eccentricity0.0006
Semi-Major Axis6,887 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2026-10-01
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-227CV
Object Type
Payload
RCS Size
Unknown
📖 About This Object
MOI-1A is an active satellite operated by India, 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. It orbits in Low Earth Orbit (LEO) at altitudes between 512 km and 520 km with an inclination of 97.4°. It travels at approximately 27,388 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.17 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 MOI-1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MOI-1A orbits at an average altitude of 516 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 MOI-1A’s average altitude, there are currently 5,772 active payloads and 280 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 30.6% of all active satellites. With an inclination of 97.4°, MOI-1A 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. India operates approximately 107 active satellites in total, of which 16 share a similar altitude band with MOI-1A.
❓ Frequently Asked Questions
MOI-1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 516 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 27,388 km/h.
MOI-1A is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 101107. You can track MOI-1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOI-1A 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 MOI-1A (NORAD ID 101107) 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.
MOI-1A travels at approximately 27,388 km/h (17,018 mph) — roughly 7.61 km/s. It completes 15.17 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.