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 46881U 94074BM 22176.38601663 .00013132 00000-0 13737-2 0 9995
2 46881 97.8884 227.2356 0008731 73.1555 287.0619 14.89737770 88760
| Epoch (UTC): | 25 June 2022 09:15:51 |
| Eccentricity: | 0.0008731 |
| inclination: | 97.8884° |
| perigee height: | 592 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 227.2356° |
| argument of perigee: | 73.1555° |
| revolutions per day: | 14.89737770 |
| mean anomaly at epoch: | 287.0619° |
| orbit number at epoch: | 8876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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