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 22179.52277697 .00000095 00000-0 47903-4 0 9991
2 39090 98.4039 17.3702 0007986 234.2111 125.8333 14.35297322488980
| Epoch (UTC): | 28 June 2022 12:32:47 |
| Eccentricity: | 0.0007986 |
| inclination: | 98.4039° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 17.3702° |
| argument of perigee: | 234.2111° |
| revolutions per day: | 14.35297322 |
| mean anomaly at epoch: | 125.8333° |
| orbit number at epoch: | 48898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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