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 59598U 26142.30044817 +.00000000 +00000-0 +00000-0 0 00001
2 59598 55.1041 101.8024 0002201 291.9380 246.4363 1.70474068 02
| Epoch (UTC): | 22 May 2026 07:12:38 |
| Eccentricity: | 0.0002201 |
| inclination: | 55.1041° |
| perigee height: | 23216 km |
| apogee height: | 23229 km |
| right ascension of ascending node: | 101.8024° |
| argument of perigee: | 291.9380° |
| revolutions per day: | 1.70474068 |
| mean anomaly at epoch: | 246.4363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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