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: 7 hours ago
TLE from 7 hours ago
0 DIWATA 2B
1 43678U 18084H 25290.98938947 .00005064 00000-0 42274-3 0 9991
2 43678 98.1074 112.2060 0007423 195.8702 164.2288 14.99020209379915Epoch: 2025-10-17T23:44Z
TLE epoch observation values (Epoch: 2025-10-17T23:44:43.250Z)
Latitude
-0.00002°
Longitude
89.29895°
Altitude
577.928 km
Speed
7.569 km/s
True Right ascension
07h 28m 49s
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
01:33:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.103 km
Perigee altitude
561.792 km
Semi-major axis
6,945.084 km
Eccentricity
0.00074
Inclination
98.1074°
RAAN
112.206°
Arg. of periapsis
195.8702°
True anomaly
164.2519°
Mean anomaly
164.2288°
Eccentric anomaly
164.24035°
Mean motion
3.74996 °/min
Orbital period
96 mins
BSTAR
0.00042274
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-18 11:07:46.545Z | 93.268° ESE | 2025-10-18 11:09:46.545Z | 59.558° ENE | 15.345° | 2025-10-18 11:11:46.545Z | 29.27° NE |
| 6 mins | 2025-10-18 12:41:46.545Z | 201.826° SSW | 2025-10-18 12:43:46.545Z | 245.668° WSW | 31.638° | 2025-10-18 12:47:46.545Z | 330.015° NNW |
| 4 mins | 2025-10-19 00:22:46.545Z | 64.005° ENE | 2025-10-19 00:23:46.545Z | 85.452° E | 22.433° | 2025-10-19 00:26:46.545Z | 144.993° SSE |
| 4 mins | 2025-10-19 01:57:46.545Z | 321.725° NNW | 2025-10-19 01:58:46.545Z | 300.947° NW | 21.438° | 2025-10-19 02:01:46.545Z | 244.141° WSW |
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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