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 23851U 26146.27101740 +.00000000 +00000-0 -41120-5 0 00007
2 23851 99.0426 83.6655 0006899 304.2984 55.7526 13.98391803 01
| Epoch (UTC): | 26 May 2026 06:30:15 |
| Eccentricity: | 0.0006899 |
| inclination: | 99.0426° |
| perigee height: | 894 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 83.6655° |
| argument of perigee: | 304.2984° |
| revolutions per day: | 13.98391803 |
| mean anomaly at epoch: | 55.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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