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 68680U 26145.43608454 +.00000000 +00000-0 +35855-3 0 00002
2 68680 97.2852 17.0685 0002640 99.9094 260.2447 15.33453557 08
| Epoch (UTC): | 25 May 2026 10:27:57 |
| Eccentricity: | 0.0002640 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.0685° |
| argument of perigee: | 99.9094° |
| revolutions per day: | 15.33453557 |
| mean anomaly at epoch: | 260.2447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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