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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Edit Public Description
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: 5 hours ago
TLE from 5 hours ago
0 DIWATA 2B
1 43678U 18084H 25322.49329329 .00003122 00000-0 26100-3 0 9994
2 43678 98.1041 144.9831 0007449 105.6548 254.5496 14.99271643384631Epoch: 2025-11-18T11:50Z
TLE epoch observation values (Epoch: 2025-11-18T11:50:20.540Z)
Latitude
-0.00003°
Longitude
-90.38107°
Altitude
573.569 km
Speed
7.573 km/s
True Right ascension
09h 39m 55s
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
13:17:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.343 km
Perigee altitude
560.997 km
Semi-major axis
6,944.307 km
Eccentricity
0.00074
Inclination
98.1041°
RAAN
144.9831°
Arg. of periapsis
105.6548°
True anomaly
254.46735°
Mean anomaly
254.5496°
Eccentric anomaly
254.50847°
Mean motion
3.75059 °/min
Orbital period
95.98 mins
BSTAR
0.000261
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-19 01:12:28.249Z | 12.921° NNE | 2025-11-19 01:16:28.249Z | 181.958° SSW | 44.939° | 2025-11-19 01:19:28.249Z | 193.544° SSW |
| 6 mins | 2025-11-19 12:00:28.249Z | 142.145° SSE | 2025-11-19 12:02:28.249Z | 99.31° ESE | 36.837° | 2025-11-19 12:06:28.249Z | 358.896° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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