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 57516U 26145.17120655 +.00000000 +00000-0 +54980-4 0 00002
2 57516 43.0058 304.0101 0001942 270.5541 89.5088 15.27584938 05
| Epoch (UTC): | 25 May 2026 04:06:32 |
| Eccentricity: | 0.0001942 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 304.0101° |
| argument of perigee: | 270.5541° |
| revolutions per day: | 15.27584938 |
| mean anomaly at epoch: | 89.5088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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