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 26039.59471920 +.00000000 +00000-0 +92459-4 0 00005
2 07735 114.9725 296.6683 0053492 292.2953 67.2463 14.25555983 03
| Epoch (UTC): | 08 February 2026 14:16:23 |
| Eccentricity: | 0.0053492 |
| inclination: | 114.9725° |
| perigee height: | 768 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 296.6683° |
| argument of perigee: | 292.2953° |
| revolutions per day: | 14.25555983 |
| mean anomaly at epoch: | 67.2463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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