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 22490U 93009B 25138.68432741 .00000532 00000-0 95119-4 0 9991
2 22490 24.9684 122.8654 0041820 283.5138 237.9471 14.45846805703957
| Epoch (UTC): | 18 May 2025 16:25:25 |
| Eccentricity: | 0.0041820 |
| inclination: | 24.9684° |
| perigee height: | 709 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 122.8654° |
| argument of perigee: | 283.5138° |
| revolutions per day: | 14.45846805 |
| mean anomaly at epoch: | 237.9471° |
| orbit number at epoch: | 70395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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