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OBJECT E

NORAD 45915 Payload LEO 2019-079E ● Active
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🛰️ Orbital Parameters
Perigee
493 km
Apogee
726 km
Inclination
97.7°
Period
96.9 min
Mean Motion
14.86245077 rev/day
TLE Epoch
2026-11-03 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude610 km
Orbital Velocity27,204 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.86
Eccentricity0.0167
Semi-Major Axis6,981 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 TsNIIKhM (Russia (CIS))
Launch Date
2019-11-25
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
2019-079E
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT E is an active satellite operated by TsNIIKhM (Russia (CIS)), launched on 2019-11-25 from Plesetsk Cosmodrome, Russia on the Nivelir? launch. Independent catalogue analysis identifies this object as Kosmos-2543 projectile, attributed to TsNIIKhM. It orbits in Low Earth Orbit (LEO) at altitudes between 493 km and 726 km with an inclination of 97.7°. It travels at approximately 27,204 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.86 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks OBJECT E 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 E orbits at an average altitude of 610 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 E’s average altitude, there are currently 1,360 active payloads and 757 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3055. This makes it one of the more crowded altitude bands, containing roughly 6.9% of all active satellites. With an inclination of 97.7°, OBJECT E passes over latitudes between 97.7°N and 97.7°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. Russia (CIS) operates approximately 1,568 active satellites in total, of which 26 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 610 km altitude. Its 97.7° 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 97 minutes, travelling at 27,204 km/h.
OBJECT E is operated by TsNIIKhM (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 45915. You can track OBJECT E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OBJECT E was launched on 2019-11-25 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 45915) 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 E travels at approximately 27,204 km/h (16,904 mph) — roughly 7.56 km/s. It completes 14.86 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.