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 68613U 26145.58335647 +.00000000 +00000-0 +47578-3 0 00000
2 68613 97.2849 345.0323 0001565 77.8279 283.0267 15.49156028 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001565 |
| inclination: | 97.2849° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.0323° |
| argument of perigee: | 77.8279° |
| revolutions per day: | 15.49156028 |
| mean anomaly at epoch: | 283.0267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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