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 22826U 93061D 22179.65885446 .00000046 00000-0 35598-4 0 9990
2 22826 98.8801 210.8117 0009154 13.0436 347.0981 14.30523603500017
| Epoch (UTC): | 28 June 2022 15:48:45 |
| Eccentricity: | 0.0009154 |
| inclination: | 98.8801° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 210.8117° |
| argument of perigee: | 13.0436° |
| revolutions per day: | 14.30523603 |
| mean anomaly at epoch: | 347.0981° |
| orbit number at epoch: | 50001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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