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: 7 hours ago
TLE from 7 hours ago
0 DIWATA 2B
1 43678U 18084H 26140.62650524 .00001835 00000-0 15146-3 0 9999
2 43678 98.1113 335.6493 0011647 265.3069 94.6823 15.00303317412086Epoch: 2026-05-20T15:02Z
TLE epoch observation values (Epoch: 2026-05-20T15:02:10.052Z)
Latitude
-0.00006°
Longitude
-128.17593°
Altitude
569.673 km
Speed
7.576 km/s
True Right ascension
22h 22m 35s
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
06:41:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.068 km
Perigee altitude
554.899 km
Semi-major axis
6,941.121 km
Eccentricity
0.00116
Inclination
98.1113°
RAAN
335.6493°
Arg. of periapsis
265.3069°
True anomaly
94.8153°
Mean anomaly
94.6823°
Eccentric anomaly
94.7488°
Mean motion
3.75317 °/min
Orbital period
95.92 mins
BSTAR
0.00015146
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-21 01:13:05.322Z | 41.199° NE | 2026-05-21 01:16:05.322Z | 97.846° ESE | 25.165° | 2026-05-21 01:19:05.322Z | 153.3° SSE |
| 4 mins | 2026-05-21 02:49:05.322Z | 326.729° NNW | 2026-05-21 02:51:05.322Z | 287.661° WNW | 19.943° | 2026-05-21 02:53:05.322Z | 251.888° W |
| 4 mins | 2026-05-21 12:01:05.322Z | 91.033° ESE | 2026-05-21 12:02:05.322Z | 73.025° E | 17.192° | 2026-05-21 12:05:05.322Z | 24.217° NE |
| 5 mins | 2026-05-21 13:35:05.322Z | 211.433° SW | 2026-05-21 13:37:05.322Z | 259.868° W | 29.037° | 2026-05-21 13:40:05.322Z | 322.243° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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