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SPAWAR-CAL-OR

NORAD 43778 Payload LEO 2018-099W ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
489 km
Apogee
502 km
Inclination
97.4°
Period
94.5 min
Mean Motion
15.23368070 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude496 km
Orbital Velocity27,429 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0009
Semi-Major Axis6,867 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099W
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SPAWAR-CAL-OR is an active satellite operated by United States, launched on 2018-12-03 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 489 km and 502 km with an inclination of 97.4°. It travels at approximately 27,429 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 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. 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 ~1–3 years. Orbital Radar tracks SPAWAR-CAL-OR in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SPAWAR-CAL-OR orbits at an average altitude of 496 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 SPAWAR-CAL-OR’s average altitude, there are currently 9,155 active payloads and 240 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.6% of all active satellites. With an inclination of 97.4°, SPAWAR-CAL-OR passes over latitudes between 97.4°N and 97.4°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 12,339 active satellites in total, of which 8,549 share a similar altitude band with SPAWAR-CAL-OR.
❓ Frequently Asked Questions
SPAWAR-CAL-OR is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 496 km altitude. Its 97.4° 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 95 minutes, travelling at 27,429 km/h.
SPAWAR-CAL-OR is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43778. You can track SPAWAR-CAL-OR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SPAWAR-CAL-OR was launched on 2018-12-03 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SPAWAR-CAL-OR (NORAD ID 43778) 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.
SPAWAR-CAL-OR travels at approximately 27,429 km/h (17,043 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.