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 26076.29921043 +.00000000 +00000-0 +55001-3 0 00007
2 23608 98.2865 281.6372 0006968 10.1505 349.9882 15.47819043 04
| Epoch (UTC): | 17 March 2026 07:10:51 |
| Eccentricity: | 0.0006968 |
| inclination: | 98.2865° |
| perigee height: | 418 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 281.6372° |
| argument of perigee: | 10.1505° |
| revolutions per day: | 15.47819043 |
| mean anomaly at epoch: | 349.9882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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