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 26037.63043473 +.00000000 +00000-0 +10555-3 0 00002
2 07735 114.9727 291.2236 0053410 292.7916 66.7530 14.25555148 06
| Epoch (UTC): | 06 February 2026 15:07:49 |
| Eccentricity: | 0.0053410 |
| inclination: | 114.9727° |
| perigee height: | 768 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 291.2236° |
| argument of perigee: | 292.7916° |
| revolutions per day: | 14.25555148 |
| mean anomaly at epoch: | 66.7530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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