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 25108.84474917 .00000016 00000-0 15728-3 0 9998
2 28538 63.8232 278.5847 0214998 279.2002 78.4766 13.43328702 48146
| Epoch (UTC): | 18 April 2025 20:16:26 |
| Eccentricity: | 0.0214998 |
| inclination: | 63.8232° |
| perigee height: | 936 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 278.5847° |
| argument of perigee: | 279.2002° |
| revolutions per day: | 13.43328702 |
| mean anomaly at epoch: | 78.4766° |
| orbit number at epoch: | 4814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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