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OBJECT A

NORAD 101228 Unknown MEO 2026-245A
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🛰️ Orbital Parameters
Perigee
178 km
Apogee
37896 km
Inclination
20.7°
Period
672.0 min
Mean Motion
2.14272993 rev/day
TLE Epoch
2026-10-30 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,037 km
Orbital Velocity14,259 km/h
Velocity3.96 km/s
Orbital Period11 hours 12 minutes
Orbits / Day2.14
Eccentricity0.7422
Semi-Major Axis25,408 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 ISRO (India)
Launch Date
2026-10-30
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2026-245A
Object Type
Unknown
RCS Size
Unknown
📖 About This Object
OBJECT A (NORAD ID 101228) is a space object catalogued under India, launched on 2026-10-30 from Satish Dhawan Space Centre, India on the IRNSS-1L launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as IRNSS-1L, attributed to ISRO. It orbits in Medium Earth Orbit (MEO) at altitudes between 178 km and 37,896 km with an inclination of 20.7°. It travels at approximately 14,259 km/h (3.96 km/s), completing one full orbit every 11 hours 12 minutes — that’s roughly 2.14 orbits per day. Its orbital eccentricity of 0.7422 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OBJECT A 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 A orbits at an average altitude of 19,037 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of OBJECT A’s average altitude, there are currently 4 active payloads and 11 tracked debris or rocket body fragments — notable neighbours include COSMOS 1413 (GLONASS), COSMOS 1415 (GLONASS), COSMOS 1521 (GLONASS). This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 20.7°, OBJECT A passes over latitudes between 20.7°N and 20.7°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. India operates approximately 108 active satellites in total.
❓ Frequently Asked Questions
OBJECT A orbits in Medium Earth Orbit (MEO) at altitudes between 178 km (perigee) and 37,896 km (apogee), with an average altitude of approximately 19,037 km. It completes one orbit every 11 hours 12 minutes, travelling at approximately 14,259 km/h (8,860 mph).
OBJECT A was launched on 2026-10-30 from Satish Dhawan Space Centre, India, India’s primary launch facility on a barrier island off the coast of Andhra Pradesh. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 101228) 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 A travels at approximately 14,259 km/h (8,860 mph) — roughly 3.96 km/s. It completes 2.14 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.