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DIWATA 2B

NORAD 43678 Payload LEO 2018-084H ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
557 km
Apogee
574 km
Inclination
98.1°
Period
96.0 min
Mean Motion
15.00459215 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude566 km
Orbital Velocity27,290 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.00
Eccentricity0.0012
Semi-Major Axis6,937 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Philippines’ Department of Science and Technology, University of the Philippines Diliman, and Japan’s Hokkaido University and Tohoku University (Philippines)
Launch Date
2018-10-29
Launch Site
TNSTA
Int'l Designator
2018-084H
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIWATA 2B is an active satellite operated by Philippines’ Department of Science and Technology, University of the Philippines Diliman, and Japan’s Hokkaido University and Tohoku University (Philippines), launched on 2018-10-29 from TNSTA. It orbits in Low Earth Orbit (LEO) at altitudes between 557 km and 574 km with an inclination of 98.1°. It travels at approximately 27,290 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.00 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 DIWATA 2B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DIWATA 2B orbits at an average altitude of 566 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 DIWATA 2B’s average altitude, there are currently 3,169 active payloads and 469 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 18.2% of all active satellites. With an inclination of 98.1°, DIWATA 2B passes over latitudes between 98.1°N and 98.1°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. Philippines operates approximately 2 active satellites in total.
❓ Frequently Asked Questions
DIWATA 2B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 566 km altitude. Its 98.1° 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 27,290 km/h.
DIWATA 2B is operated by Philippines’ Department of Science and Technology, University of the Philippines Diliman, and Japan’s Hokkaido University and Tohoku University (Philippines). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43678. You can track DIWATA 2B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DIWATA 2B was launched on 2018-10-29 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIWATA 2B (NORAD ID 43678) 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.
DIWATA 2B travels at approximately 27,290 km/h (16,957 mph) — roughly 7.58 km/s. It completes 15.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.