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 26140.54703479 +.00000000 +00000-0 +18326-3 0 00007
2 23851 99.0421 78.0228 0006996 323.0446 37.0235 13.98390241 05
| Epoch (UTC): | 20 May 2026 13:07:43 |
| Eccentricity: | 0.0006996 |
| inclination: | 99.0421° |
| perigee height: | 894 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 78.0228° |
| argument of perigee: | 323.0446° |
| revolutions per day: | 13.98390241 |
| mean anomaly at epoch: | 37.0235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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