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STEP 2

NORAD 23105 Payload LEO 1994-029A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
538 km
Apogee
651 km
Inclination
81.9°
Period
96.6 min
Mean Motion
14.91099548 rev/day
TLE Epoch
2026-09-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude595 km
Orbital Velocity27,233 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.91
Eccentricity0.0081
Semi-Major Axis6,966 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF STP (United States)
Launch Date
1994-05-19
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1994-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
STEP 2 is an active satellite operated by USAF STP (United States), launched on 1994-05-19 from Vandenberg Space Force Base, United States on the STEP 2 launch. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 538 km and 651 km with an inclination of 81.9°. It travels at approximately 27,233 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.91 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks STEP 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
STEP 2 orbits at an average altitude of 595 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 STEP 2’s average altitude, there are currently 1,674 active payloads and 680 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 9% of all active satellites. With an inclination of 81.9°, STEP 2 passes over latitudes between 81.9°N and 81.9°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. United States operates approximately 13,204 active satellites in total, of which 1,077 share a similar altitude band with STEP 2.
❓ Frequently Asked Questions
STEP 2 orbits in Low Earth Orbit (LEO) at altitudes between 538 km (perigee) and 651 km (apogee), with an average altitude of approximately 595 km. It completes one orbit every 97 minutes, travelling at approximately 27,233 km/h (16,922 mph).
STEP 2 is operated by USAF STP (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23105. You can track STEP 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
STEP 2 was launched on 1994-05-19 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 STEP 2 (NORAD ID 23105) 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.
STEP 2 travels at approximately 27,233 km/h (16,922 mph) — roughly 7.56 km/s. It completes 14.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.