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 23093U 26042.05179767 +.00000000 +00000-0 +90857-4 0 00009
2 23093 82.9440 282.5818 0010840 136.9392 223.2616 13.78226445 00
| Epoch (UTC): | 11 February 2026 01:14:35 |
| Eccentricity: | 0.0010840 |
| inclination: | 82.9440° |
| perigee height: | 962 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 282.5818° |
| argument of perigee: | 136.9392° |
| revolutions per day: | 13.78226445 |
| mean anomaly at epoch: | 223.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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