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 43678U 18084H 22179.11159468 .00000262 00000-0 31533-4 0 9994
2 43678 97.9719 312.5024 0008503 247.3912 112.6410 14.92184013199448
| Epoch (UTC): | 28 June 2022 02:40:41 |
| Eccentricity: | 0.0008503 |
| inclination: | 97.9719° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 312.5024° |
| argument of perigee: | 247.3912° |
| revolutions per day: | 14.92184013 |
| mean anomaly at epoch: | 112.6410° |
| orbit number at epoch: | 19944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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