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 22147.61537137 .00008406 00000-0 16439-2 0 9996
2 00085 38.7688 353.8201 0372962 199.2866 159.3431 14.26734461 32107
| Epoch (UTC): | 27 May 2022 14:46:08 |
| Eccentricity: | 0.0372962 |
| inclination: | 38.7688° |
| perigee height: | 535 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 353.8201° |
| argument of perigee: | 199.2866° |
| revolutions per day: | 14.26734461 |
| mean anomaly at epoch: | 159.3431° |
| orbit number at epoch: | 3210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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