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 13028U 82001B 22222.80431385 .00000058 00000-0 27651-4 0 9995
2 13028 74.0419 163.8975 0019013 143.6356 216.6094 14.38536057127530
| Epoch (UTC): | 10 August 2022 19:18:12 |
| Eccentricity: | 0.0019013 |
| inclination: | 74.0419° |
| perigee height: | 750 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 163.8975° |
| argument of perigee: | 143.6356° |
| revolutions per day: | 14.38536057 |
| mean anomaly at epoch: | 216.6094° |
| orbit number at epoch: | 12753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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