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 22176.09402148 .00000718 00000-0 76246-4 0 9990
2 43678 97.9717 309.4490 0008447 258.0952 101.9277 14.92184735198990
| Epoch (UTC): | 25 June 2022 02:15:23 |
| Eccentricity: | 0.0008447 |
| inclination: | 97.9717° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 309.4490° |
| argument of perigee: | 258.0952° |
| revolutions per day: | 14.92184735 |
| mean anomaly at epoch: | 101.9277° |
| orbit number at epoch: | 19899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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