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 23087.50075244 .00000685 00000-0 25261-3 0 9999
2 39090 98.3927 283.0603 0009717 139.7478 220.4429 14.35520741528141
| Epoch (UTC): | 28 March 2023 12:01:05 |
| Eccentricity: | 0.0009717 |
| inclination: | 98.3927° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 283.0603° |
| argument of perigee: | 139.7478° |
| revolutions per day: | 14.35520741 |
| mean anomaly at epoch: | 220.4429° |
| orbit number at epoch: | 52814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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