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 23091.90930285 .00000297 00000-0 13147-3 0 9997
2 22826 98.8458 133.4007 0007857 277.3322 82.6967 14.30632635539654
| Epoch (UTC): | 01 April 2023 21:49:23 |
| Eccentricity: | 0.0007857 |
| inclination: | 98.8458° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 133.4007° |
| argument of perigee: | 277.3322° |
| revolutions per day: | 14.30632635 |
| mean anomaly at epoch: | 82.6967° |
| orbit number at epoch: | 53965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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