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 68914U 26145.26205902 +.00000000 +00000-0 +88468-3 0 00002
2 68914 97.2861 340.9632 0002187 77.3725 282.7771 15.49207776 01
| Epoch (UTC): | 25 May 2026 06:17:21 |
| Eccentricity: | 0.0002187 |
| inclination: | 97.2861° |
| perigee height: | 418 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 340.9632° |
| argument of perigee: | 77.3725° |
| revolutions per day: | 15.49207776 |
| mean anomaly at epoch: | 282.7771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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