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 22825U 93061C 25082.94335137 .00000498 00000-0 20757-3 0 9995
2 22825 98.7458 144.0818 0008016 348.1247 11.9745 14.30758031642610
| Epoch (UTC): | 23 March 2025 22:38:25 |
| Eccentricity: | 0.0008016 |
| inclination: | 98.7458° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 144.0818° |
| argument of perigee: | 348.1247° |
| revolutions per day: | 14.30758031 |
| mean anomaly at epoch: | 11.9745° |
| orbit number at epoch: | 64261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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