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 38254U 12019A 25136.66063918 -.00000122 00000-0 00000-0 0 9997
2 38254 5.7333 60.1241 0002745 357.2899 38.4942 1.00270336 3016
| Epoch (UTC): | 16 May 2025 15:51:19 |
| Eccentricity: | 0.0002745 |
| inclination: | 5.7333° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 60.1241° |
| argument of perigee: | 357.2899° |
| revolutions per day: | 1.00270336 |
| mean anomaly at epoch: | 38.4942° |
| orbit number at epoch: | 301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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