View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 17912U 87038B 25198.37012436 .00000370 00000-0 40436-4 0 9998
2 17912 82.5026 158.4060 0018306 218.5974 141.3935 14.85061736 44301
| Epoch (UTC): | 17 July 2025 08:52:58 |
| Eccentricity: | 0.0018306 |
| inclination: | 82.5026° |
| perigee height: | 600 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 158.4060° |
| argument of perigee: | 218.5974° |
| revolutions per day: | 14.85061736 |
| mean anomaly at epoch: | 141.3935° |
| orbit number at epoch: | 4430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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