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 57647U 26145.35657941 +.00000000 +00000-0 +63601-4 0 00000
2 57647 43.0010 19.3985 0001271 274.8339 85.2368 15.27586649 06
| Epoch (UTC): | 25 May 2026 08:33:28 |
| Eccentricity: | 0.0001271 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.3985° |
| argument of perigee: | 274.8339° |
| revolutions per day: | 15.27586649 |
| mean anomaly at epoch: | 85.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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