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PROVES-ELECTRA

NORAD 69799 Payload LEO 1998-067YP ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
408 km
Apogee
422 km
Inclination
51.6°
Period
92.9 min
Mean Motion
15.50565584 rev/day
TLE Epoch
2026-07-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude415 km
Orbital Velocity27,591 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.51
Eccentricity0.0010
Semi-Major Axis6,786 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1998-11-20
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1998-067YP
Object Type
Payload
RCS Size
Unknown
📖 About This Object
PROVES-ELECTRA is an active satellite operated by United States, launched on 1998-11-20 from Baikonur, 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 408 km and 422 km with an inclination of 51.6°. It travels at approximately 27,591 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.51 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. 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 415 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of PROVES-ELECTRA’s average altitude, there are currently 2,706 active payloads and 110 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 15.3% 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 12,566 active satellites in total, of which 2,515 share a similar altitude band with PROVES-ELECTRA.
❓ Frequently Asked Questions
PROVES-ELECTRA orbits in Low Earth Orbit (LEO) at altitudes between 408 km (perigee) and 422 km (apogee), with an average altitude of approximately 415 km. It completes one orbit every 93 minutes, travelling at approximately 27,591 km/h (17,144 mph).
PROVES-ELECTRA is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69799. 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, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks PROVES-ELECTRA (NORAD ID 69799) 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 27,591 km/h (17,144 mph) — roughly 7.66 km/s. It completes 15.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.