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 26304.19317060 .00001202 00000-0 99581-4 0 9992
2 43678 98.1136 146.3825 0013123 83.7880 276.4837 15.00863566436618Epoch: 2026-10-31T04:38Z
TLE epoch observation values (Epoch: 2026-10-31T04:38:09.939Z)
Latitude
-0.00007°
Longitude
37.33869°
Altitude
566.258 km
Speed
7.579 km/s
True Right ascension
09h 45m 31s
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
10:12:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.361 km
Perigee altitude
552.148 km
Semi-major axis
6,939.392 km
Eccentricity
0.00131
Inclination
98.1136°
RAAN
146.3825°
Arg. of periapsis
83.788°
True anomaly
276.33426°
Mean anomaly
276.4837°
Eccentric anomaly
276.40898°
Mean motion
3.75458 °/min
Orbital period
95.88 mins
BSTAR
0.000099581
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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 | 2026-11-01 02:00:45.353Z | 36.38° NE | 2026-11-01 02:03:45.353Z | 101.509° ESE | 35.706° | 2026-11-01 02:06:45.353Z | 161.855° S |
| 4 mins | 2026-11-01 03:36:45.353Z | 321.333° NNW | 2026-11-01 03:38:45.353Z | 285.997° WNW | 16.607° | 2026-11-01 03:40:45.353Z | 255.217° W |
| 5 mins | 2026-11-01 12:47:45.353Z | 106.695° ESE | 2026-11-01 12:49:45.353Z | 67.819° E | 22.14° | 2026-11-01 12:52:45.353Z | 17.778° NNE |
| 5 mins | 2026-11-01 14:22:45.353Z | 223.448° SW | 2026-11-01 14:24:45.353Z | 268.494° W | 25.985° | 2026-11-01 14:27:45.353Z | 319.898° 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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