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 68493U 26145.32869959 +.00000000 +00000-0 +41690-3 0 00005
2 68493 97.7638 103.9292 0005650 97.1545 263.0316 14.91405913 03
| Epoch (UTC): | 25 May 2026 07:53:19 |
| Eccentricity: | 0.0005650 |
| inclination: | 97.7638° |
| perigee height: | 590 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.9292° |
| argument of perigee: | 97.1545° |
| revolutions per day: | 14.91405913 |
| mean anomaly at epoch: | 263.0316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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