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 39090U 13009E 22176.80400035 .00000119 00000-0 56444-4 0 9990
2 39090 98.4042 14.7227 0007890 243.4506 116.5871 14.35296494488591
| Epoch (UTC): | 25 June 2022 19:17:45 |
| Eccentricity: | 0.0007890 |
| inclination: | 98.4042° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 14.7227° |
| argument of perigee: | 243.4506° |
| revolutions per day: | 14.35296494 |
| mean anomaly at epoch: | 116.5871° |
| orbit number at epoch: | 48859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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