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 26040.74503122 +.00000000 +00000-0 +87095-4 0 00009
2 23093 82.9442 283.5549 0010772 140.3089 219.8859 13.78226187 03
| Epoch (UTC): | 09 February 2026 17:52:50 |
| Eccentricity: | 0.0010772 |
| inclination: | 82.9442° |
| perigee height: | 962 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 283.5549° |
| argument of perigee: | 140.3089° |
| revolutions per day: | 13.78226187 |
| mean anomaly at epoch: | 219.8859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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