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 43772U 18099Q 25138.16960852 .00026134 00000-0 90537-3 0 9999
2 43772 97.4723 203.0377 0004859 163.9512 196.1883 15.29812411353575
| Epoch (UTC): | 18 May 2025 04:04:14 |
| Eccentricity: | 0.0004859 |
| inclination: | 97.4723° |
| perigee height: | 473 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 203.0377° |
| argument of perigee: | 163.9512° |
| revolutions per day: | 15.29812411 |
| mean anomaly at epoch: | 196.1883° |
| orbit number at epoch: | 35357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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