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 20442U 90005G 23089.42350096 .00000523 00000-0 20675-3 0 9990
2 20442 98.8368 64.2889 0012680 53.0806 307.1537 14.33212452734122
| Epoch (UTC): | 30 March 2023 10:09:50 |
| Eccentricity: | 0.0012680 |
| inclination: | 98.8368° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 64.2889° |
| argument of perigee: | 53.0806° |
| revolutions per day: | 14.33212452 |
| mean anomaly at epoch: | 307.1537° |
| orbit number at epoch: | 73412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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