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 56887U 26145.33148441 +.00000000 +00000-0 -79235-4 0 00004
2 56887 43.0029 16.4683 0001053 267.5155 92.5576 15.27586829 09
| Epoch (UTC): | 25 May 2026 07:57:20 |
| Eccentricity: | 0.0001053 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 16.4683° |
| argument of perigee: | 267.5155° |
| revolutions per day: | 15.27586829 |
| mean anomaly at epoch: | 92.5576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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