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MONOLITH

NORAD 49052 Payload LEO 2021-068A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
536 km
Apogee
541 km
Inclination
37.0°
Period
95.4 min
Mean Motion
15.09169902 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude539 km
Orbital Velocity27,343 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.09
Eccentricity0.0004
Semi-Major Axis6,910 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Air Force Research Laboratory (United States)
Launch Date
2021-07-29
Launch Site
RLLC
Int'l Designator
2021-068A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
MONOLITH is an active satellite operated by Air Force Research Laboratory (United States), launched on 2021-07-29 from RLLC. It orbits in Low Earth Orbit (LEO) at altitudes between 536 km and 541 km with an inclination of 37.0°. It travels at approximately 27,343 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.09 orbits per day. 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 ~3–10 years. Orbital Radar tracks MONOLITH in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MONOLITH orbits at an average altitude of 539 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 MONOLITH’s average altitude, there are currently 3,496 active payloads and 325 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 37.0°, MONOLITH passes over latitudes between 37.0°N and 37.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 12,339 active satellites in total, of which 2,823 share a similar altitude band with MONOLITH.
❓ Frequently Asked Questions
MONOLITH orbits in Low Earth Orbit (LEO) at altitudes between 536 km (perigee) and 541 km (apogee), with an average altitude of approximately 539 km. It completes one orbit every 95 minutes, travelling at approximately 27,343 km/h (16,990 mph).
MONOLITH is operated by Air Force Research Laboratory (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 49052. You can track MONOLITH in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MONOLITH was launched on 2021-07-29 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks MONOLITH (NORAD ID 49052) 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.
MONOLITH travels at approximately 27,343 km/h (16,990 mph) — roughly 7.60 km/s. It completes 15.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.