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 45760U 26145.58335647 +.00000000 +00000-0 +45088-3 0 00002
2 45760 53.0381 123.3934 0005045 40.4715 252.3854 15.97933534 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005045 |
| inclination: | 53.0381° |
| perigee height: | 277 km |
| apogee height: | 284 km |
| right ascension of ascending node: | 123.3934° |
| argument of perigee: | 40.4715° |
| revolutions per day: | 15.97933534 |
| mean anomaly at epoch: | 252.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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