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 28069U 99057MZ 24356.57263866 .00003079 00000-0 74850-3 0 9994
2 28069 98.5505 39.3535 0070891 319.7178 39.8776 14.52077525626853
| Epoch (UTC): | 21 December 2024 13:44:35 |
| Eccentricity: | 0.0070891 |
| inclination: | 98.5505° |
| perigee height: | 668 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 39.3535° |
| argument of perigee: | 319.7178° |
| revolutions per day: | 14.52077525 |
| mean anomaly at epoch: | 39.8776° |
| orbit number at epoch: | 62685 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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