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 07714U 26064.24379003 +.00000000 +00000-0 +56856-4 0 00002
2 07714 81.1961 331.0201 0027808 284.3695 75.4388 14.08462402 05
| Epoch (UTC): | 05 March 2026 05:51:03 |
| Eccentricity: | 0.0027808 |
| inclination: | 81.1961° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 331.0201° |
| argument of perigee: | 284.3695° |
| revolutions per day: | 14.08462402 |
| mean anomaly at epoch: | 75.4388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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