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 68424U 26145.33901878 +.00000000 +00000-0 +26290-3 0 00006
2 68424 97.4506 104.1134 0003869 103.7617 256.4048 15.18099155 05
| Epoch (UTC): | 25 May 2026 08:08:11 |
| Eccentricity: | 0.0003869 |
| inclination: | 97.4506° |
| perigee height: | 509 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 104.1134° |
| argument of perigee: | 103.7617° |
| revolutions per day: | 15.18099155 |
| mean anomaly at epoch: | 256.4048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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