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 28647U 05016B 25194.39428233 .00010108 00000-0 29886-3 0 9990
2 28647 56.9993 187.7278 0069122 284.4420 74.8966 15.33254626340244
| Epoch (UTC): | 13 July 2025 09:27:45 |
| Eccentricity: | 0.0069122 |
| inclination: | 56.9993° |
| perigee height: | 419 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 187.7278° |
| argument of perigee: | 284.4420° |
| revolutions per day: | 15.33254626 |
| mean anomaly at epoch: | 74.8966° |
| orbit number at epoch: | 34024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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