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 25509U 98061B 18175.90352049 .00000165 00000-0 21846-4 0 9996
2 25509 31.4315 111.0331 0346578 33.6799 328.5349 14.30336827 27549
| Epoch (UTC): | 24 June 2018 21:41:04 |
| Eccentricity: | 0.0346578 |
| inclination: | 31.4315° |
| perigee height: | 542 km |
| apogee height: | 1039 km |
| right ascension of ascending node: | 111.0331° |
| argument of perigee: | 33.6799° |
| revolutions per day: | 14.30336827 |
| mean anomaly at epoch: | 328.5349° |
| orbit number at epoch: | 2754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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