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 00085U 61004C 22220.39225895 .00004391 00000-0 84869-3 0 9990
2 00085 38.7699 338.6923 0373200 328.6050 29.2902 14.27641187 42506
| Epoch (UTC): | 08 August 2022 09:24:51 |
| Eccentricity: | 0.0373200 |
| inclination: | 38.7699° |
| perigee height: | 532 km |
| apogee height: | 1067 km |
| right ascension of ascending node: | 338.6923° |
| argument of perigee: | 328.6050° |
| revolutions per day: | 14.27641187 |
| mean anomaly at epoch: | 29.2902° |
| orbit number at epoch: | 4250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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