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 26065U 26039.17699066 +.00000000 +00000-0 +10603-3 0 00009
2 26065 100.1913 315.8746 0036480 39.0120 321.3683 14.38174839 00
| Epoch (UTC): | 08 February 2026 04:14:51 |
| Eccentricity: | 0.0036480 |
| inclination: | 100.1913° |
| perigee height: | 738 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 315.8746° |
| argument of perigee: | 39.0120° |
| revolutions per day: | 14.38174839 |
| mean anomaly at epoch: | 321.3683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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