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 68714U 26145.41090527 +.00000000 +00000-0 +10238-2 0 00001
2 68714 53.1595 38.1294 0000596 84.7985 275.3092 15.49357486 04
| Epoch (UTC): | 25 May 2026 09:51:42 |
| Eccentricity: | 0.0000596 |
| inclination: | 53.1595° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 38.1294° |
| argument of perigee: | 84.7985° |
| revolutions per day: | 15.49357486 |
| mean anomaly at epoch: | 275.3092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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