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 is defined by the following mean orbital elements,
1 43553U 98067PB 21094.62928569 .03890718 12239-4 60024-3 0 9995
2 43553 51.6239 227.0840 0009894 313.2518 46.7680 16.33102743156209
| Epoch (UTC): | 04 April 2021 15:06:10 |
| Eccentricity: | 0.0009894 |
| inclination: | 51.6239° |
| perigee height: | 178 km |
| apogee height: | 191 km |
| right ascension of ascending node: | 227.0840° |
| argument of perigee: | 313.2518° |
| revolutions per day: | 16.33102743 |
| mean anomaly at epoch: | 46.7680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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