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 20440U 90005E 22176.89368330 .00000085 00000-0 47392-4 0 9994
2 20440 98.8192 148.9203 0011479 140.1021 274.5783 14.33334424694216
| Epoch (UTC): | 25 June 2022 21:26:54 |
| Eccentricity: | 0.0011479 |
| inclination: | 98.8192° |
| perigee height: | 772 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 148.9203° |
| argument of perigee: | 140.1021° |
| revolutions per day: | 14.33334424 |
| mean anomaly at epoch: | 274.5783° |
| orbit number at epoch: | 69421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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