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 68477U 26145.32910819 +.00000000 +00000-0 +70736-3 0 00002
2 68477 97.7508 103.8503 0005832 125.8686 234.3075 14.91564520 05
| Epoch (UTC): | 25 May 2026 07:53:54 |
| Eccentricity: | 0.0005832 |
| inclination: | 97.7508° |
| perigee height: | 589 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.8503° |
| argument of perigee: | 125.8686° |
| revolutions per day: | 14.91564520 |
| mean anomaly at epoch: | 234.3075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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