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 22146.28552036 .00010249 00000-0 20024-2 0 9996
2 00085 38.7684 0.6702 0372826 190.3350 168.9565 14.26710299 31910
| Epoch (UTC): | 26 May 2022 06:51:08 |
| Eccentricity: | 0.0372826 |
| inclination: | 38.7684° |
| perigee height: | 535 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 0.6702° |
| argument of perigee: | 190.3350° |
| revolutions per day: | 14.26710299 |
| mean anomaly at epoch: | 168.9565° |
| orbit number at epoch: | 3191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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