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 28646U 05016A 22068.15671116 0.00000000 00000-0 00000-0 0 07
2 28646 57.0118 166.2790 0007131 74.4171 285.5829 14.51876129 00
| Epoch (UTC): | 09 March 2022 03:45:39 |
| Eccentricity: | 0.0007131 |
| inclination: | 57.0118° |
| perigee height: | 714 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 166.2790° |
| argument of perigee: | 74.4171° |
| revolutions per day: | 14.51876129 |
| mean anomaly at epoch: | 285.5829° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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