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 22272.85127991 .00005632 00000-0 10756-2 0 9998
2 00085 38.7689 68.0006 0372044 321.5512 35.9260 14.28073530 50008
| Epoch (UTC): | 29 September 2022 20:25:50 |
| Eccentricity: | 0.0372044 |
| inclination: | 38.7689° |
| perigee height: | 531 km |
| apogee height: | 1065 km |
| right ascension of ascending node: | 68.0006° |
| argument of perigee: | 321.5512° |
| revolutions per day: | 14.28073530 |
| mean anomaly at epoch: | 35.9260° |
| orbit number at epoch: | 5000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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