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 28307U 91082U 24277.88848713 .00000623 00000-0 37366-3 0 9998
2 28307 98.8670 316.9035 0039016 168.6019 5.0602 14.10211237 52201
| Epoch (UTC): | 03 October 2024 21:19:25 |
| Eccentricity: | 0.0039016 |
| inclination: | 98.8670° |
| perigee height: | 830 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 316.9035° |
| argument of perigee: | 168.6019° |
| revolutions per day: | 14.10211237 |
| mean anomaly at epoch: | 5.0602° |
| orbit number at epoch: | 5220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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