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 39026U 12072A 19264.10284284 .00000898 00000-0 34808-4 0 9995
2 39026 97.2144 264.2157 0039403 124.1277 236.3710 15.27992698376016
| Epoch (UTC): | 21 September 2019 02:28:05 |
| Eccentricity: | 0.0039403 |
| inclination: | 97.2144° |
| perigee height: | 455 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 264.2157° |
| argument of perigee: | 124.1277° |
| revolutions per day: | 15.27992698 |
| mean anomaly at epoch: | 236.3710° |
| orbit number at epoch: | 37601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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