FIREFLY-2
NORAD 62704
Payload
LEO
2025-009CZ
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LEO · NORAD 62704
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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
584 km
Apogee
594 km
Inclination
97.7°
Period
96.5 min
Mean Motion
14.92678393 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude589 km
Orbital Velocity27,244 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.93
Eccentricity0.0007
Semi-Major Axis6,960 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2025-01-14
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-009CZ
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
FIREFLY-2 is an active satellite operated by India, launched on 2025-01-14 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 584 km and 594 km with an inclination of 97.7°. It travels at approximately 27,244 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.93 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 ~3–10 years. Orbital Radar tracks FIREFLY-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
FIREFLY-2 orbits at an average altitude of 589 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 FIREFLY-2’s average altitude, there are currently 3,168 active payloads and 601 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 18.2% of all active satellites. With an inclination of 97.7°, FIREFLY-2 passes over latitudes between 97.7°N and 97.7°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. India operates approximately 108 active satellites in total, of which 16 share a similar altitude band with FIREFLY-2.
❓ Frequently Asked Questions
FIREFLY-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 589 km altitude. Its 97.7° 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 27,244 km/h.
FIREFLY-2 is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 62704. You can track FIREFLY-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FIREFLY-2 was launched on 2025-01-14 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 FIREFLY-2 (NORAD ID 62704) 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.
FIREFLY-2 travels at approximately 27,244 km/h (16,928 mph) — roughly 7.57 km/s. It completes 14.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.