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 45859U 26145.28573580 +.00000000 +00000-0 +51478-4 0 00009
2 45859 98.1848 156.8409 0127639 298.4727 60.3665 14.60918963 04
| Epoch (UTC): | 25 May 2026 06:51:27 |
| Eccentricity: | 0.0127639 |
| inclination: | 98.1848° |
| perigee height: | 600 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 156.8409° |
| argument of perigee: | 298.4727° |
| revolutions per day: | 14.60918963 |
| mean anomaly at epoch: | 60.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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