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 45344U 26145.59932851 +.00000000 +00000-0 +00000-0 0 00003
2 45344 2.8208 47.0202 0002487 11.8283 120.1289 1.00271081 04
| Epoch (UTC): | 25 May 2026 14:23:01 |
| Eccentricity: | 0.0002487 |
| inclination: | 2.8208° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 47.0202° |
| argument of perigee: | 11.8283° |
| revolutions per day: | 1.00271081 |
| mean anomaly at epoch: | 120.1289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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