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 00020U 26108.10063523 +.00000000 +00000-0 +13479-3 0 00009
2 00020 33.3391 123.2741 1637393 91.4570 287.3327 11.61924474 05
| Epoch (UTC): | 18 April 2026 02:24:54 |
| Eccentricity: | 0.1637393 |
| inclination: | 33.3391° |
| perigee height: | 508 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 123.2741° |
| argument of perigee: | 91.4570° |
| revolutions per day: | 11.61924474 |
| mean anomaly at epoch: | 287.3327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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