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 28538U 05004B 24277.79063352 .00000097 00000-0 28088-3 0 9997
2 28538 63.8252 55.8587 0210692 290.3451 67.5054 13.43281093 21695
| Epoch (UTC): | 03 October 2024 18:58:30 |
| Eccentricity: | 0.0210692 |
| inclination: | 63.8252° |
| perigee height: | 939 km |
| apogee height: | 1254 km |
| right ascension of ascending node: | 55.8587° |
| argument of perigee: | 290.3451° |
| revolutions per day: | 13.43281093 |
| mean anomaly at epoch: | 67.5054° |
| orbit number at epoch: | 2169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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