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 43145U 18005A 26005.68602539 0.00000000 00000-0 00000-0 0 06
2 43145 106.0138 86.2685 0001000 81.5333 278.4666 13.48042969 02
| Epoch (UTC): | 05 January 2026 16:27:52 |
| Eccentricity: | 0.0001000 |
| inclination: | 106.0138° |
| perigee height: | 1079 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 86.2685° |
| argument of perigee: | 81.5333° |
| revolutions per day: | 13.48042969 |
| mean anomaly at epoch: | 278.4666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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