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 25173.57454102 .00000064 00000-0 41763-4 0 9999
2 22825 98.7360 235.1947 0009509 77.3597 282.8648 14.30803387655849
| Epoch (UTC): | 22 June 2025 13:47:20 |
| Eccentricity: | 0.0009509 |
| inclination: | 98.7360° |
| perigee height: | 782 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 235.1947° |
| argument of perigee: | 77.3597° |
| revolutions per day: | 14.30803387 |
| mean anomaly at epoch: | 282.8648° |
| orbit number at epoch: | 65584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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