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 43116U 18004F 21023.75614132 .00001397 00000-0 59591-4 0 9998
2 43116 97.4305 99.5470 0009015 1.8915 358.2355 15.24566998168593
| Epoch (UTC): | 23 January 2021 18:08:50 |
| Eccentricity: | 0.0009015 |
| inclination: | 97.4305° |
| perigee height: | 486 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 99.5470° |
| argument of perigee: | 1.8915° |
| revolutions per day: | 15.24566998 |
| mean anomaly at epoch: | 358.2355° |
| orbit number at epoch: | 16859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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