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 35865U 26103.18264480 +.00000000 +00000-0 +44868-4 0 00009
2 35865 98.7329 66.1451 0003104 120.9717 239.1766 14.23141939 06
| Epoch (UTC): | 13 April 2026 04:23:00 |
| Eccentricity: | 0.0003104 |
| inclination: | 98.7329° |
| perigee height: | 813 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 66.1451° |
| argument of perigee: | 120.9717° |
| revolutions per day: | 14.23141939 |
| mean anomaly at epoch: | 239.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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