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N2-P-BODY

NORAD 69929 Payload LEO 2026-156BN ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
583 km
Apogee
597 km
Inclination
97.8°
Period
96.5 min
Mean Motion
14.92490399 rev/day
TLE Epoch
2026-08-08 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude590 km
Orbital Velocity27,242 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.92
Eccentricity0.0010
Semi-Major Axis6,961 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-07-07
Launch Site
Vandenberg SFB, California
Int'l Designator
2026-156BN
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
N2-P-BODY is an active satellite operated by United States, launched on 2026-07-07 from Vandenberg SFB, California on the Transporter-17 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 583 km and 597 km with an inclination of 97.8°. It travels at approximately 27,242 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.92 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 ~3–10 years. Orbital Radar tracks N2-P-BODY in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
N2-P-BODY orbits at an average altitude of 590 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 N2-P-BODY’s average altitude, there are currently 2,219 active payloads and 605 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 12.4% of all active satellites. With an inclination of 97.8°, N2-P-BODY passes over latitudes between 97.8°N and 97.8°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 12,712 active satellites in total, of which 1,647 share a similar altitude band with N2-P-BODY.
❓ Frequently Asked Questions
N2-P-BODY is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 590 km altitude. Its 97.8° 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 96 minutes, travelling at 27,242 km/h.
N2-P-BODY is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69929. You can track N2-P-BODY in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
N2-P-BODY was launched on 2026-07-07 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 N2-P-BODY (NORAD ID 69929) 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.
N2-P-BODY travels at approximately 27,242 km/h (16,927 mph) — roughly 7.57 km/s. It completes 14.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.