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 43678U 26101.27463471 +.00000000 +00000-0 +16081-3 0 00004
2 43678 98.1050 294.6517 0013965 31.7230 328.4830 15.00135457 06
| Epoch (UTC): | 11 April 2026 06:35:28 |
| Eccentricity: | 0.0013965 |
| inclination: | 98.1050° |
| perigee height: | 557 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 294.6517° |
| argument of perigee: | 31.7230° |
| revolutions per day: | 15.00135457 |
| mean anomaly at epoch: | 328.4830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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