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 24282.55516426 .00000136 00000-0 34067-3 0 9990
2 28538 63.8264 43.8365 0210860 290.0670 67.7775 13.43282801 22338
| Epoch (UTC): | 08 October 2024 13:19:26 |
| Eccentricity: | 0.0210860 |
| inclination: | 63.8264° |
| perigee height: | 939 km |
| apogee height: | 1254 km |
| right ascension of ascending node: | 43.8365° |
| argument of perigee: | 290.0670° |
| revolutions per day: | 13.43282801 |
| mean anomaly at epoch: | 67.7775° |
| orbit number at epoch: | 2233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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