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 22487U 93008A 25108.56478661 .00000066 00000-0 52159-4 0 9990
2 22487 82.9426 137.5910 0037055 220.6387 252.9643 13.75994194611922
| Epoch (UTC): | 18 April 2025 13:33:17 |
| Eccentricity: | 0.0037055 |
| inclination: | 82.9426° |
| perigee height: | 951 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 137.5910° |
| argument of perigee: | 220.6387° |
| revolutions per day: | 13.75994194 |
| mean anomaly at epoch: | 252.9643° |
| orbit number at epoch: | 61192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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