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 is defined by the following mean orbital elements,
1 15945U 26100.18187609 +.00000000 +00000-0 +48441-4 0 00001
2 15945 82.5298 355.3292 0020362 88.1762 272.1787 14.86468599 08
| Epoch (UTC): | 10 April 2026 04:21:54 |
| Eccentricity: | 0.0020362 |
| inclination: | 82.5298° |
| perigee height: | 595 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 355.3292° |
| argument of perigee: | 88.1762° |
| revolutions per day: | 14.86468599 |
| mean anomaly at epoch: | 272.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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