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 23589U 26146.03666200 +.00000000 +00000-0 +00000-0 0 00002
2 23589 11.9986 10.4005 0003652 355.6435 17.9502 0.98752458 02
| Epoch (UTC): | 26 May 2026 00:52:47 |
| Eccentricity: | 0.0003652 |
| inclination: | 11.9986° |
| perigee height: | 36202 km |
| apogee height: | 36234 km |
| right ascension of ascending node: | 10.4005° |
| argument of perigee: | 355.6435° |
| revolutions per day: | 0.98752458 |
| mean anomaly at epoch: | 17.9502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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