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 24281.43847820 .00000071 00000-0 24111-3 0 9998
2 28538 63.8260 46.6539 0210854 290.1252 67.7202 13.43281943 22160
| Epoch (UTC): | 07 October 2024 10:31:24 |
| Eccentricity: | 0.0210854 |
| inclination: | 63.8260° |
| perigee height: | 939 km |
| apogee height: | 1254 km |
| right ascension of ascending node: | 46.6539° |
| argument of perigee: | 290.1252° |
| revolutions per day: | 13.43281943 |
| mean anomaly at epoch: | 67.7202° |
| orbit number at epoch: | 2216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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