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 68478U 26145.36422926 +.00000000 +00000-0 +10209-3 0 00003
2 68478 97.7588 104.0002 0002588 39.3219 320.8187 14.92094344 05
| Epoch (UTC): | 25 May 2026 08:44:29 |
| Eccentricity: | 0.0002588 |
| inclination: | 97.7588° |
| perigee height: | 590 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 104.0002° |
| argument of perigee: | 39.3219° |
| revolutions per day: | 14.92094344 |
| mean anomaly at epoch: | 320.8187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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