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 68456U 26145.63535617 +.00000000 +00000-0 +27721-3 0 00008
2 68456 97.4538 104.3523 0007051 129.7592 230.4264 15.17238770 05
| Epoch (UTC): | 25 May 2026 15:14:54 |
| Eccentricity: | 0.0007051 |
| inclination: | 97.4538° |
| perigee height: | 509 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 104.3523° |
| argument of perigee: | 129.7592° |
| revolutions per day: | 15.17238770 |
| mean anomaly at epoch: | 230.4264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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