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 59600U 26145.12607097 +.00000000 +00000-0 +00000-0 0 00003
2 59600 55.1013 101.7225 0001702 32.8778 327.0916 1.70474148 04
| Epoch (UTC): | 25 May 2026 03:01:32 |
| Eccentricity: | 0.0001702 |
| inclination: | 55.1013° |
| perigee height: | 23217 km |
| apogee height: | 23227 km |
| right ascension of ascending node: | 101.7225° |
| argument of perigee: | 32.8778° |
| revolutions per day: | 1.70474148 |
| mean anomaly at epoch: | 327.0916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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