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 21797U 91081B 23270.78824708 .00000135 00000-0 11948-3 0 9998
2 21797 82.9557 158.5888 0038637 139.6732 286.0505 13.77637562600161
| Epoch (UTC): | 27 September 2023 18:55:04 |
| Eccentricity: | 0.0038637 |
| inclination: | 82.9557° |
| perigee height: | 944 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 158.5888° |
| argument of perigee: | 139.6732° |
| revolutions per day: | 13.77637562 |
| mean anomaly at epoch: | 286.0505° |
| orbit number at epoch: | 60016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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