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 26044.97256582 +.00000000 +00000-0 +17027-3 0 00001
2 43678 98.1055 236.0349 0009383 200.3036 159.7815 14.99840409 06
| Epoch (UTC): | 13 February 2026 23:20:29 |
| Eccentricity: | 0.0009383 |
| inclination: | 98.1055° |
| perigee height: | 561 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 236.0349° |
| argument of perigee: | 200.3036° |
| revolutions per day: | 14.99840409 |
| mean anomaly at epoch: | 159.7815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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