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 26064.74106191 +.00000000 +00000-0 +55078-4 0 00008
2 07714 81.1959 330.5347 0027824 282.9123 76.8939 14.08462462 08
| Epoch (UTC): | 05 March 2026 17:47:07 |
| Eccentricity: | 0.0027824 |
| inclination: | 81.1959° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 330.5347° |
| argument of perigee: | 282.9123° |
| revolutions per day: | 14.08462462 |
| mean anomaly at epoch: | 76.8939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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