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 07659U 26100.13713397 +.00000000 +00000-0 +28847-3 0 00005
2 07659 49.8159 1.3722 0185248 104.5323 257.6201 13.94054088 01
| Epoch (UTC): | 10 April 2026 03:17:28 |
| Eccentricity: | 0.0185248 |
| inclination: | 49.8159° |
| perigee height: | 779 km |
| apogee height: | 1050 km |
| right ascension of ascending node: | 1.3722° |
| argument of perigee: | 104.5323° |
| revolutions per day: | 13.94054088 |
| mean anomaly at epoch: | 257.6201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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