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 38771U 12049A 25080.85782592 .00000415 00000-0 20952-3 0 9994
2 38771 98.5877 137.2809 0000880 141.5851 218.5390 14.21458192648994
| Epoch (UTC): | 21 March 2025 20:35:16 |
| Eccentricity: | 0.0000880 |
| inclination: | 98.5877° |
| perigee height: | 820 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 137.2809° |
| argument of perigee: | 141.5851° |
| revolutions per day: | 14.21458192 |
| mean anomaly at epoch: | 218.5390° |
| orbit number at epoch: | 64899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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