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 45679U 26145.08141690 +.00000000 +00000-0 +98693-3 0 00009
2 45679 53.0422 26.2525 0006792 109.2846 250.8902 15.63054357 00
| Epoch (UTC): | 25 May 2026 01:57:14 |
| Eccentricity: | 0.0006792 |
| inclination: | 53.0422° |
| perigee height: | 374 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 26.2525° |
| argument of perigee: | 109.2846° |
| revolutions per day: | 15.63054357 |
| mean anomaly at epoch: | 250.8902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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