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 68331U 26145.58332184 +.00000000 +00000-0 +83007-3 0 00007
2 68331 53.1597 347.1624 0001387 96.6949 263.4212 15.35391579 00
| Epoch (UTC): | 25 May 2026 13:59:59 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.1597° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 347.1624° |
| argument of perigee: | 96.6949° |
| revolutions per day: | 15.35391579 |
| mean anomaly at epoch: | 263.4212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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