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 23608U 26065.75865904 +.00000000 +00000-0 +90411-3 0 00003
2 23608 98.2875 269.5732 0007439 46.4427 313.7437 15.46919036 06
| Epoch (UTC): | 06 March 2026 18:12:28 |
| Eccentricity: | 0.0007439 |
| inclination: | 98.2875° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 269.5732° |
| argument of perigee: | 46.4427° |
| revolutions per day: | 15.46919036 |
| mean anomaly at epoch: | 313.7437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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