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 43669U 18083H 22280.44538742 .00015470 00000-0 65170-3 0 9998
2 43669 97.4091 303.5809 0007852 305.9586 190.0992 15.23407182218347
| Epoch (UTC): | 07 October 2022 10:41:21 |
| Eccentricity: | 0.0007852 |
| inclination: | 97.4091° |
| perigee height: | 490 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 303.5809° |
| argument of perigee: | 305.9586° |
| revolutions per day: | 15.23407182 |
| mean anomaly at epoch: | 190.0992° |
| orbit number at epoch: | 21834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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