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 57745U 26145.26977624 +.00000000 +00000-0 +48701-4 0 00006
2 57745 43.0034 100.3699 0000499 249.6829 110.3969 15.27559542 08
| Epoch (UTC): | 25 May 2026 06:28:28 |
| Eccentricity: | 0.0000499 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 100.3699° |
| argument of perigee: | 249.6829° |
| revolutions per day: | 15.27559542 |
| mean anomaly at epoch: | 110.3969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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