LEMUR 2 EMBRIONOVIS
NORAD 56970
Payload
LEO
2023-084AQ
● Active
CONNECTING…
LEO · NORAD 56970
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
448 km
Apogee
459 km
Inclination
97.6°
Period
93.7 min
Mean Motion
15.37582970 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude454 km
Orbital Velocity27,513 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.38
Eccentricity0.0008
Semi-Major Axis6,825 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Spire Global (United States)
Launch Date
2023-06-12
Launch Site
Vandenberg SFB, California
Int'l Designator
2023-084AQ
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR 2 EMBRIONOVIS is an active satellite operated by Spire Global (United States), launched on 2023-06-12 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 448 km and 459 km with an inclination of 97.6°. It travels at approximately 27,513 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.38 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 LEMUR 2 EMBRIONOVIS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LEMUR 2 EMBRIONOVIS orbits at an average altitude of 454 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 LEMUR 2 EMBRIONOVIS’s average altitude, there are currently 7,790 active payloads and 169 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 44.7% of all active satellites. With an inclination of 97.6°, LEMUR 2 EMBRIONOVIS passes over latitudes between 97.6°N and 97.6°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 7,359 share a similar altitude band with LEMUR 2 EMBRIONOVIS.
🔗 Spire Global Constellation
This satellite is part of Spire Global's constellation of 3U CubeSats collecting weather, maritime and aviation data through radio occultation, AIS and ADS-B payloads. Spire operates over 100 multi-purpose nanosatellites in LEO, providing atmospheric profiles used by weather agencies worldwide, global ship tracking and flight tracking services.
❓ Frequently Asked Questions
LEMUR 2 EMBRIONOVIS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 454 km altitude. Its 97.6° 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 94 minutes, travelling at 27,513 km/h.
LEMUR 2 EMBRIONOVIS is operated by Spire Global (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 56970. You can track LEMUR 2 EMBRIONOVIS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR 2 EMBRIONOVIS was launched on 2023-06-12 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 LEMUR 2 EMBRIONOVIS (NORAD ID 56970) 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.
LEMUR 2 EMBRIONOVIS travels at approximately 27,513 km/h (17,096 mph) — roughly 7.64 km/s. It completes 15.38 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.