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 57063U 26145.39407833 +.00000000 +00000-0 +18895-2 0 00002
2 57063 43.0023 37.4396 0001109 273.2494 86.8231 15.27319494 02
| Epoch (UTC): | 25 May 2026 09:27:28 |
| Eccentricity: | 0.0001109 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 37.4396° |
| argument of perigee: | 273.2494° |
| revolutions per day: | 15.27319494 |
| mean anomaly at epoch: | 86.8231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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