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 23156.08485181 .00000315 00000-0 12401-3 0 9996
2 39090 98.3890 349.7787 0007886 305.6577 54.3874 14.35595686538006
| Epoch (UTC): | 05 June 2023 02:02:11 |
| Eccentricity: | 0.0007886 |
| inclination: | 98.3890° |
| perigee height: | 767 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 349.7787° |
| argument of perigee: | 305.6577° |
| revolutions per day: | 14.35595686 |
| mean anomaly at epoch: | 54.3874° |
| orbit number at epoch: | 53800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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