PROVES-ELECTRA
NORAD 69795
Payload
LEO
1998-067YK
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LEO · NORAD 69795
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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
388 km
Apogee
399 km
Inclination
51.6°
Period
92.4 min
Mean Motion
15.58016554 rev/day
TLE Epoch
2026-09-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude394 km
Orbital Velocity27,635 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.58
Eccentricity0.0008
Semi-Major Axis6,765 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 UCSC (United States)
Launch Date
1998-11-20
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1998-067YK
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PROVES-ELECTRA is an active satellite operated by UCSC (United States), launched on 1998-11-20 from Baikonur Cosmodrome, Kazakhstan on the 77KM No. 17501 launch. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 388 km and 399 km with an inclination of 51.6°. It travels at approximately 27,635 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.58 orbits per day. 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 months to ~1 year. Orbital Radar tracks PROVES-ELECTRA in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PROVES-ELECTRA orbits at an average altitude of 394 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of PROVES-ELECTRA’s average altitude, there are currently 1,357 active payloads and 82 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 7.3% of all active satellites. With an inclination of 51.6°, PROVES-ELECTRA passes over latitudes between 51.6°N and 51.6°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,196 active satellites in total, of which 1,205 share a similar altitude band with PROVES-ELECTRA.
❓ Frequently Asked Questions
PROVES-ELECTRA orbits in Low Earth Orbit (LEO) at altitudes between 388 km (perigee) and 399 km (apogee), with an average altitude of approximately 394 km. It completes one orbit every 92 minutes, travelling at approximately 27,635 km/h (17,171 mph).
PROVES-ELECTRA is operated by UCSC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69795. You can track PROVES-ELECTRA in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PROVES-ELECTRA was launched on 1998-11-20 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks PROVES-ELECTRA (NORAD ID 69795) 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.
PROVES-ELECTRA travels at approximately 27,635 km/h (17,171 mph) — roughly 7.68 km/s. It completes 15.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.