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 07735U 26042.19037918 +.00000000 +00000-0 +86346-4 0 00008
2 07735 114.9725 303.8627 0053569 291.6454 67.8928 14.25557132 06
| Epoch (UTC): | 11 February 2026 04:34:08 |
| Eccentricity: | 0.0053569 |
| inclination: | 114.9725° |
| perigee height: | 768 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 303.8627° |
| argument of perigee: | 291.6454° |
| revolutions per day: | 14.25557132 |
| mean anomaly at epoch: | 67.8928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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