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: 9 hours ago
TLE from 9 hours ago
0 DIWATA 2B
1 43678U 18084H 25308.94454751 .00002099 00000-0 17772-3 0 9993
2 43678 98.1086 130.8874 0007956 139.7689 220.4123 14.99164463382603Epoch: 2025-11-04T22:40Z
TLE epoch observation values (Epoch: 2025-11-04T22:40:08.904Z)
Latitude
-0.00004°
Longitude
106.426°
Altitude
576.729 km
Speed
7.57 km/s
True Right ascension
08h 43m 32s
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
04:07:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.027 km
Perigee altitude
560.976 km
Semi-major axis
6,944.638 km
Eccentricity
0.0008
Inclination
98.1086°
RAAN
130.8874°
Arg. of periapsis
139.7689°
True anomaly
220.35324°
Mean anomaly
220.4123°
Eccentric anomaly
220.38277°
Mean motion
3.75032 °/min
Orbital period
95.99 mins
BSTAR
0.00017772
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-05 11:37:39.227Z | 125.353° SE | 2025-11-05 11:40:39.227Z | 62.018° ENE | 26.731° | 2025-11-05 11:43:39.227Z | 10.488° NNE |
| 4 mins | 2025-11-05 13:13:39.227Z | 232.435° WSW | 2025-11-05 13:15:39.227Z | 269.148° W | 18.1° | 2025-11-05 13:17:39.227Z | 303.474° NW |
| 6 mins | 2025-11-06 00:52:39.227Z | 28.751° NE | 2025-11-06 00:55:39.227Z | 117.779° SE | 37.878° | 2025-11-06 00:58:39.227Z | 175.488° S |
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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