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 26390U 26145.29706307 +.00000000 +00000-0 +00000-0 0 00005
2 26390 59.3827 160.3741 0003887 300.4695 236.9904 1.57877313 06
| Epoch (UTC): | 25 May 2026 07:07:46 |
| Eccentricity: | 0.0003887 |
| inclination: | 59.3827° |
| perigee height: | 24764 km |
| apogee height: | 24789 km |
| right ascension of ascending node: | 160.3741° |
| argument of perigee: | 300.4695° |
| revolutions per day: | 1.57877313 |
| mean anomaly at epoch: | 236.9904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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