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 57833U 26145.62520786 +.00000000 +00000-0 +79683-4 0 00000
2 57833 85.9903 269.3403 0002528 112.5939 247.5511 14.12444251 09
| Epoch (UTC): | 25 May 2026 15:00:17 |
| Eccentricity: | 0.0002528 |
| inclination: | 85.9903° |
| perigee height: | 849 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 269.3403° |
| argument of perigee: | 112.5939° |
| revolutions per day: | 14.12444251 |
| mean anomaly at epoch: | 247.5511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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