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 10657U 26063.51422197 +.00000000 +00000-0 -27189-4 0 00002
2 10657 102.5952 47.1659 0083157 242.6725 231.3091 12.25775359 04
| Epoch (UTC): | 04 March 2026 12:20:28 |
| Eccentricity: | 0.0083157 |
| inclination: | 102.5952° |
| perigee height: | 1501 km |
| apogee height: | 1634 km |
| right ascension of ascending node: | 47.1659° |
| argument of perigee: | 242.6725° |
| revolutions per day: | 12.25775359 |
| mean anomaly at epoch: | 231.3091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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