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 45460U 26145.64160321 +.00000000 +00000-0 +20794-3 0 00008
2 45460 34.9960 348.2854 0003522 202.1258 157.9299 15.02586599 00
| Epoch (UTC): | 25 May 2026 15:23:54 |
| Eccentricity: | 0.0003522 |
| inclination: | 34.9960° |
| perigee height: | 556 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 348.2854° |
| argument of perigee: | 202.1258° |
| revolutions per day: | 15.02586599 |
| mean anomaly at epoch: | 157.9299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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