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 23855U 96026A 25093.29630790 0.00000000 00000-0 00000-0 0 04
2 23855 8.1336 353.2659 0334621 300.1447 56.3921 1.00270000 03
| Epoch (UTC): | 03 April 2025 07:06:41 |
| Eccentricity: | 0.0334621 |
| inclination: | 8.1336° |
| perigee height: | 34376 km |
| apogee height: | 37197 km |
| right ascension of ascending node: | 353.2659° |
| argument of perigee: | 300.1447° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 56.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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