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 40358U 26145.60427667 +.00000000 +00000-0 +39635-3 0 00008
2 40358 67.1534 62.2372 0008478 263.5289 96.4831 13.97821660 06
| Epoch (UTC): | 25 May 2026 14:30:09 |
| Eccentricity: | 0.0008478 |
| inclination: | 67.1534° |
| perigee height: | 895 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 62.2372° |
| argument of perigee: | 263.5289° |
| revolutions per day: | 13.97821660 |
| mean anomaly at epoch: | 96.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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