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 68241U 26145.46161898 +.00000000 +00000-0 +70367-3 0 00001
2 68241 53.1581 300.4798 0001454 96.4133 263.7033 15.30206036 07
| Epoch (UTC): | 25 May 2026 11:04:43 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.4798° |
| argument of perigee: | 96.4133° |
| revolutions per day: | 15.30206036 |
| mean anomaly at epoch: | 263.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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