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 08682U 75004J 22222.47531158 .00000209 00000-0 10585-3 0 9997
2 08682 97.7329 39.8087 0153852 285.7271 72.6984 14.18434090450722
| Epoch (UTC): | 10 August 2022 11:24:26 |
| Eccentricity: | 0.0153852 |
| inclination: | 97.7329° |
| perigee height: | 720 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 39.8087° |
| argument of perigee: | 285.7271° |
| revolutions per day: | 14.18434090 |
| mean anomaly at epoch: | 72.6984° |
| orbit number at epoch: | 45072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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