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 38745U 12044B 25114.52945833 .00071192 53014-5 13795-2 0 9995
2 38745 49.8458 301.8726 1729210 149.9104 221.3579 12.07367456509468
| Epoch (UTC): | 24 April 2025 12:42:25 |
| Eccentricity: | 0.1729210 |
| inclination: | 49.8458° |
| perigee height: | 260 km |
| apogee height: | 3036 km |
| right ascension of ascending node: | 301.8726° |
| argument of perigee: | 149.9104° |
| revolutions per day: | 12.07367456 |
| mean anomaly at epoch: | 221.3579° |
| orbit number at epoch: | 50946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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