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 42065U 17011B 26002.73672907 0.00000000 00000-0 00000-0 0 01
2 42065 63.4339 213.5410 0158555 359.6793 0.2286 13.40990564 03
| Epoch (UTC): | 02 January 2026 17:40:53 |
| Eccentricity: | 0.0158555 |
| inclination: | 63.4339° |
| perigee height: | 987 km |
| apogee height: | 1224 km |
| right ascension of ascending node: | 213.5410° |
| argument of perigee: | 359.6793° |
| revolutions per day: | 13.40990564 |
| mean anomaly at epoch: | 0.2286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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