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 23561U 26088.20601934 +.00000000 +00000-0 +12802-3 0 00005
2 23561 98.4463 159.4209 0007905 86.2381 335.0168 14.39786488 06
| Epoch (UTC): | 29 March 2026 04:56:40 |
| Eccentricity: | 0.0007905 |
| inclination: | 98.4463° |
| perigee height: | 754 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 159.4209° |
| argument of perigee: | 86.2381° |
| revolutions per day: | 14.39786488 |
| mean anomaly at epoch: | 335.0168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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