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: 10 hours ago
TLE from 10 hours ago
0 DIWATA 2B
1 43678U 18084H 25352.59123101 .00002365 00000-0 19800-3 0 9995
2 43678 98.1019 176.2889 0007622 31.5778 328.5900 14.99466484389144Epoch: 2025-12-18T14:11Z
TLE epoch observation values (Epoch: 2025-12-18T14:11:22.359Z)
Latitude
-0°
Longitude
-123.9988°
Altitude
567.067 km
Speed
7.58 km/s
True Right ascension
11h 45m 09s
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
23:29:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.86 km
Perigee altitude
560.275 km
Semi-major axis
6,943.705 km
Eccentricity
0.00076
Inclination
98.1019°
RAAN
176.2889°
Arg. of periapsis
31.5778°
True anomaly
328.54444°
Mean anomaly
328.59°
Eccentric anomaly
328.56723°
Mean motion
3.75108 °/min
Orbital period
95.97 mins
BSTAR
0.000198
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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 | 2025-12-19 01:57:07.279Z | 352.065° N | 2025-12-19 02:01:07.279Z | 275.972° WNW | 27.084° | 2025-12-19 02:04:07.279Z | 227.599° WSW |
| 5 mins | 2025-12-19 12:45:07.279Z | 192.83° SSW | 2025-12-19 12:47:07.279Z | 253.615° W | 38.356° | 2025-12-19 12:50:07.279Z | 332.522° NNW |
| 4 mins | 2025-12-20 00:25:07.279Z | 61.033° ENE | 2025-12-20 00:27:07.279Z | 97.41° ESE | 18.075° | 2025-12-20 00:29:07.279Z | 131.983° SE |
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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