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 19649U 88102A 23159.47781214 .00000334 00000-0 19791-3 0 9992
2 19649 70.9985 165.1270 0007320 245.8082 114.2275 14.14842400782942
| Epoch (UTC): | 08 June 2023 11:28:02 |
| Eccentricity: | 0.0007320 |
| inclination: | 70.9985° |
| perigee height: | 837 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 165.1270° |
| argument of perigee: | 245.8082° |
| revolutions per day: | 14.14842400 |
| mean anomaly at epoch: | 114.2275° |
| orbit number at epoch: | 78294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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