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 02765U 26033.04571132 +.00000000 +00000-0 +00000-0 0 00000
2 02765 40.2332 8.7346 5059430 289.1160 358.9814 0.21528609 08
| Epoch (UTC): | 02 February 2026 01:05:49 |
| Eccentricity: | 0.5059430 |
| inclination: | 40.2332° |
| perigee height: | 51721 km |
| apogee height: | 170714 km |
| right ascension of ascending node: | 8.7346° |
| argument of perigee: | 289.1160° |
| revolutions per day: | 0.21528609 |
| mean anomaly at epoch: | 358.9814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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