DIWATA 2B, 43678
Orbit data source: Space-Track
DIWATA 2B, 43678 is a Filipino payload satellite in SSO that was launched on Mon, 29 Oct 2018 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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43678 intel report (Beta)
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Identifier
Orbit
Country
RPRelated business
Manufacturer
UPD/HOKK
Mission
Operational Civil Imaging
Bus & Motor
DIWATA, Unknown motor
Mass
56 kg wet, 56 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.514 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 DIWATA 2B
1 43678U 18084H 26123.95256792 .00003701 00000-0 30057-3 0 9997
2 43678 98.1071 318.2733 0012671 323.5658 36.4701 15.00235881409582Epoch: 2026-05-03T22:51Z
TLE epoch observation values (Epoch: 2026-05-03T22:51:41.868Z)
Latitude
-0°
Longitude
113.50012°
Altitude
562.137 km
Speed
7.584 km/s
True Right ascension
21h 13m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.987 km
Perigee altitude
554.396 km
Semi-major axis
6,941.329 km
Eccentricity
0.00127
Inclination
98.1071°
RAAN
318.2733°
Arg. of periapsis
323.5658°
True anomaly
36.55652°
Mean anomaly
36.4701°
Eccentric anomaly
36.5133°
Mean motion
3.75301 °/min
Orbital period
95.92 mins
BSTAR
0.00030057
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Other satellites on launch #84 in the year 2018 (2018-10-29 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DIWATA 2B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-04 13:24:31.230Z | 204.723° SW | 2026-05-04 13:26:31.230Z | 259.74° W | 32.872° | 2026-05-04 13:29:31.230Z | 326.702° NNW |
| 4 mins | 2026-05-05 01:04:31.230Z | 63.263° ENE | 2026-05-05 01:06:31.230Z | 107.141° ESE | 21.708° | 2026-05-05 01:08:31.230Z | 142.346° SSE |
| 4 mins | 2026-05-05 02:39:31.230Z | 323.008° NNW | 2026-05-05 02:40:31.230Z | 301.85° NW | 22.523° | 2026-05-05 02:43:31.230Z | 243.133° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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