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 22285U 92093B 25199.18123968 -.00000250 00000-0 -10365-3 0 9993
2 22285 71.0218 136.5450 0006366 293.2113 66.8339 14.15400571680294
| Epoch (UTC): | 18 July 2025 04:20:59 |
| Eccentricity: | 0.0006366 |
| inclination: | 71.0218° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 136.5450° |
| argument of perigee: | 293.2113° |
| revolutions per day: | 14.15400571 |
| mean anomaly at epoch: | 66.8339° |
| orbit number at epoch: | 68029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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