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 00045U 60007A 22146.76867316 .00000559 00000-0 16688-3 0 9992
2 00045 66.6945 314.1275 0252566 161.6572 199.3847 14.33845103167371
| Epoch (UTC): | 26 May 2022 18:26:53 |
| Eccentricity: | 0.0252566 |
| inclination: | 66.6945° |
| perigee height: | 598 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 314.1275° |
| argument of perigee: | 161.6572° |
| revolutions per day: | 14.33845103 |
| mean anomaly at epoch: | 199.3847° |
| orbit number at epoch: | 16737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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