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 68500U 26145.31960675 +.00000000 +00000-0 +21667-3 0 00002
2 68500 97.7607 103.9184 0003817 91.1101 269.0555 14.91540476 08
| Epoch (UTC): | 25 May 2026 07:40:14 |
| Eccentricity: | 0.0003817 |
| inclination: | 97.7607° |
| perigee height: | 590 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 103.9184° |
| argument of perigee: | 91.1101° |
| revolutions per day: | 14.91540476 |
| mean anomaly at epoch: | 269.0555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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