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 23088.47657151 .00000765 00000-0 28042-3 0 9998
2 39090 98.3926 284.0097 0009762 137.0268 223.1682 14.35522671528286
| Epoch (UTC): | 29 March 2023 11:26:15 |
| Eccentricity: | 0.0009762 |
| inclination: | 98.3926° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 284.0097° |
| argument of perigee: | 137.0268° |
| revolutions per day: | 14.35522671 |
| mean anomaly at epoch: | 223.1682° |
| orbit number at epoch: | 52828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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