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 13403U 82079B 22221.80566137 .00001122 00000-0 69907-4 0 9993
2 13403 81.1654 274.4396 0030968 191.0690 168.9857 15.08392472179849
| Epoch (UTC): | 09 August 2022 19:20:09 |
| Eccentricity: | 0.0030968 |
| inclination: | 81.1654° |
| perigee height: | 519 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 274.4396° |
| argument of perigee: | 191.0690° |
| revolutions per day: | 15.08392472 |
| mean anomaly at epoch: | 168.9857° |
| orbit number at epoch: | 17984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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