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 25196.91972005 -.00000234 00000-0 -95393-4 0 9992
2 22285 71.0217 141.2918 0006360 295.6359 64.4107 14.15401397679659
| Epoch (UTC): | 15 July 2025 22:04:23 |
| Eccentricity: | 0.0006360 |
| inclination: | 71.0217° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 141.2918° |
| argument of perigee: | 295.6359° |
| revolutions per day: | 14.15401397 |
| mean anomaly at epoch: | 64.4107° |
| orbit number at epoch: | 67965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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