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 39765U 26106.98070277 +.00000000 +00000-0 +81260-4 0 00009
2 39765 82.4461 293.7383 0232192 145.1430 216.5133 12.82902133 01
| Epoch (UTC): | 16 April 2026 23:32:12 |
| Eccentricity: | 0.0232192 |
| inclination: | 82.4461° |
| perigee height: | 1151 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 293.7383° |
| argument of perigee: | 145.1430° |
| revolutions per day: | 12.82902133 |
| mean anomaly at epoch: | 216.5133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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