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 24358.03689265 -.00000120 00000-0 -36976-4 0 9993
2 22285 71.0203 211.3449 0006721 264.5202 95.5154 14.15346554650980
| Epoch (UTC): | 23 December 2024 00:53:07 |
| Eccentricity: | 0.0006721 |
| inclination: | 71.0203° |
| perigee height: | 836 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 211.3449° |
| argument of perigee: | 264.5202° |
| revolutions per day: | 14.15346554 |
| mean anomaly at epoch: | 95.5154° |
| orbit number at epoch: | 65098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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