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 68471U 26145.33356564 +.00000000 +00000-0 +51084-3 0 00003
2 68471 97.7561 103.8755 0005387 113.8036 246.3748 14.91308267 02
| Epoch (UTC): | 25 May 2026 08:00:20 |
| Eccentricity: | 0.0005387 |
| inclination: | 97.7561° |
| perigee height: | 590 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 103.8755° |
| argument of perigee: | 113.8036° |
| revolutions per day: | 14.91308267 |
| mean anomaly at epoch: | 246.3748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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