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 26070U 26137.75600764 +.00000000 +00000-0 -55124-4 0 00004
2 26070 71.0018 312.6126 0014433 74.6692 285.6024 14.15830793 02
| Epoch (UTC): | 17 May 2026 18:08:39 |
| Eccentricity: | 0.0014433 |
| inclination: | 71.0018° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 312.6126° |
| argument of perigee: | 74.6692° |
| revolutions per day: | 14.15830793 |
| mean anomaly at epoch: | 285.6024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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