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 57289U 26145.61570977 +.00000000 +00000-0 +46913-4 0 00001
2 57289 86.5047 12.5977 0014533 250.2228 109.7348 13.39549415 07
| Epoch (UTC): | 25 May 2026 14:46:37 |
| Eccentricity: | 0.0014533 |
| inclination: | 86.5047° |
| perigee height: | 1100 km |
| apogee height: | 1122 km |
| right ascension of ascending node: | 12.5977° |
| argument of perigee: | 250.2228° |
| revolutions per day: | 13.39549415 |
| mean anomaly at epoch: | 109.7348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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