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 23088U 26022.34092409 +.00000000 +00000-0 +14407-4 0 00007
2 23088 70.9999 168.2225 0003929 329.1082 30.9809 14.15007075 09
| Epoch (UTC): | 22 January 2026 08:10:55 |
| Eccentricity: | 0.0003929 |
| inclination: | 70.9999° |
| perigee height: | 839 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 168.2225° |
| argument of perigee: | 329.1082° |
| revolutions per day: | 14.15007075 |
| mean anomaly at epoch: | 30.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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