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 28931U 06002A 21127.85863949 .00000128 00000-0 33816-4 0 9992
2 28931 97.8849 104.3849 0001917 102.3247 257.8174 14.62832855815121
| Epoch (UTC): | 07 May 2021 20:36:26 |
| Eccentricity: | 0.0001917 |
| inclination: | 97.8849° |
| perigee height: | 682 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 104.3849° |
| argument of perigee: | 102.3247° |
| revolutions per day: | 14.62832855 |
| mean anomaly at epoch: | 257.8174° |
| orbit number at epoch: | 81512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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