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 68058U 26145.18472905 +.00000000 +00000-0 +50339-3 0 00007
2 68058 53.1575 54.3225 0001011 112.8359 247.2749 15.30207746 08
| Epoch (UTC): | 25 May 2026 04:26:00 |
| Eccentricity: | 0.0001011 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.3225° |
| argument of perigee: | 112.8359° |
| revolutions per day: | 15.30207746 |
| mean anomaly at epoch: | 247.2749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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