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 16953U 86070B 22139.75265938 .00000247 00000-0 91293-4 0 9998
2 16953 74.0121 203.9851 0012534 350.5074 9.5840 14.37504414870327
| Epoch (UTC): | 19 May 2022 18:03:49 |
| Eccentricity: | 0.0012534 |
| inclination: | 74.0121° |
| perigee height: | 758 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 203.9851° |
| argument of perigee: | 350.5074° |
| revolutions per day: | 14.37504414 |
| mean anomaly at epoch: | 9.5840° |
| orbit number at epoch: | 87032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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