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 28973U 79095J 24276.59237677 .00035564 00000-0 12669-1 0 9994
2 28973 81.2050 11.7960 0022343 190.4209 169.6515 14.33904342982072
| Epoch (UTC): | 02 October 2024 14:13:01 |
| Eccentricity: | 0.0022343 |
| inclination: | 81.2050° |
| perigee height: | 763 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 11.7960° |
| argument of perigee: | 190.4209° |
| revolutions per day: | 14.33904342 |
| mean anomaly at epoch: | 169.6515° |
| orbit number at epoch: | 98207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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