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 23696U 26146.16815858 +.00000000 +00000-0 +00000-0 0 00000
2 23696 11.5292 14.8797 0003623 176.2252 184.3419 0.98762855 03
| Epoch (UTC): | 26 May 2026 04:02:08 |
| Eccentricity: | 0.0003623 |
| inclination: | 11.5292° |
| perigee height: | 36200 km |
| apogee height: | 36230 km |
| right ascension of ascending node: | 14.8797° |
| argument of perigee: | 176.2252° |
| revolutions per day: | 0.98762855 |
| mean anomaly at epoch: | 184.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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