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 25201.52607556 -.00000065 00000-0 33130-4 0 9997
2 28538 63.8244 44.6828 0215901 273.8910 83.7462 13.43339262 60614
| Epoch (UTC): | 20 July 2025 12:37:32 |
| Eccentricity: | 0.0215901 |
| inclination: | 63.8244° |
| perigee height: | 935 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 44.6828° |
| argument of perigee: | 273.8910° |
| revolutions per day: | 13.43339262 |
| mean anomaly at epoch: | 83.7462° |
| orbit number at epoch: | 6061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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