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 25134.52761241 .00000016 00000-0 15640-3 0 9994
2 28538 63.8241 213.7691 0215372 277.7239 79.9384 13.43332870 51592
| Epoch (UTC): | 14 May 2025 12:39:45 |
| Eccentricity: | 0.0215372 |
| inclination: | 63.8241° |
| perigee height: | 936 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 213.7691° |
| argument of perigee: | 277.7239° |
| revolutions per day: | 13.43332870 |
| mean anomaly at epoch: | 79.9384° |
| orbit number at epoch: | 5159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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