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 07734U 26160.08395661 +.00000000 +00000-0 +38845-4 0 00009
2 07734 114.9886 258.3155 0022907 297.3780 62.4968 14.19182723 08
| Epoch (UTC): | 09 June 2026 02:00:53 |
| Eccentricity: | 0.0022907 |
| inclination: | 114.9886° |
| perigee height: | 812 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 258.3155° |
| argument of perigee: | 297.3780° |
| revolutions per day: | 14.19182723 |
| mean anomaly at epoch: | 62.4968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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