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 22178.54680599 .00000108 00000-0 52766-4 0 9999
2 39090 98.4039 16.4198 0007950 237.4980 122.5438 14.35297076488840
| Epoch (UTC): | 27 June 2022 13:07:24 |
| Eccentricity: | 0.0007950 |
| inclination: | 98.4039° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 16.4198° |
| argument of perigee: | 237.4980° |
| revolutions per day: | 14.35297076 |
| mean anomaly at epoch: | 122.5438° |
| orbit number at epoch: | 48884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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