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 26088.15132067 +.00000000 +00000-0 +17869-3 0 00003
2 23093 82.9425 248.2415 0010364 20.6399 339.5176 13.78241119 09
| Epoch (UTC): | 29 March 2026 03:37:54 |
| Eccentricity: | 0.0010364 |
| inclination: | 82.9425° |
| perigee height: | 963 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 248.2415° |
| argument of perigee: | 20.6399° |
| revolutions per day: | 13.78241119 |
| mean anomaly at epoch: | 339.5176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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