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 25140.55748963 -.00000039 00000-0 73058-4 0 9994
2 28538 63.8231 198.5520 0215467 277.3749 80.2842 13.43333690 52427
| Epoch (UTC): | 20 May 2025 13:22:47 |
| Eccentricity: | 0.0215467 |
| inclination: | 63.8231° |
| perigee height: | 936 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 198.5520° |
| argument of perigee: | 277.3749° |
| revolutions per day: | 13.43333690 |
| mean anomaly at epoch: | 80.2842° |
| orbit number at epoch: | 5242 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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