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 data is extracted from the following two-line orbital elements,
1 28230U 04014A 25340.93959326 .00001719 00000-0 21015-3 0 9994
2 28230 89.8456 53.9219 0001882 94.1442 265.9998 14.82908820623853
| Epoch (UTC): | 06 December 2025 22:33:00 |
| Eccentricity: | 0.0001882 |
| inclination: | 89.8456° |
| perigee height: | 619 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 53.9219° |
| argument of perigee: | 94.1442° |
| revolutions per day: | 14.82908820 |
| mean anomaly at epoch: | 265.9998° |
| orbit number at epoch: | 62385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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