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 23159.53927372 .00000161 00000-0 78993-4 0 9995
2 22826 98.8359 202.1536 0010096 80.9483 279.2841 14.30667484549320
| Epoch (UTC): | 08 June 2023 12:56:33 |
| Eccentricity: | 0.0010096 |
| inclination: | 98.8359° |
| perigee height: | 782 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 202.1536° |
| argument of perigee: | 80.9483° |
| revolutions per day: | 14.30667484 |
| mean anomaly at epoch: | 279.2841° |
| orbit number at epoch: | 54932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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