STEP 2
NORAD 23105
Payload
LEO
1994-029A
● Active
CONNECTING…
LEO · NORAD 23105
NOW PASSING OVER
Calculating position…
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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
539 km
Apogee
652 km
Inclination
81.9°
Period
96.6 min
Mean Motion
14.90727056 rev/day
TLE Epoch
2026-06-19 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude596 km
Orbital Velocity27,231 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.91
Eccentricity0.0081
Semi-Major Axis6,967 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-05-19
Launch Site
Vandenberg SFB, California
Int'l Designator
1994-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
STEP 2 is an active satellite operated by United States, launched on 1994-05-19 from Vandenberg SFB, California. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 539 km and 652 km with an inclination of 81.9°. It travels at approximately 27,231 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 596 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 2,115 active payloads and 634 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 12.1% 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 12,360 active satellites in total, of which 1,569 share a similar altitude band with STEP 2.
❓ Frequently Asked Questions
STEP 2 orbits in Low Earth Orbit (LEO) at altitudes between 539 km (perigee) and 652 km (apogee), with an average altitude of approximately 596 km. It completes one orbit every 97 minutes, travelling at approximately 27,231 km/h (16,921 mph).
STEP 2 is operated by 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 SFB, California, 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 27,231 km/h (16,921 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.