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 00046U 60007B 21340.66891634 .00000062 00000-0 35553-4 0 9999
2 00046 66.6918 34.7661 0202379 90.7166 271.7134 14.49478548216960
| Epoch (UTC): | 06 December 2021 16:03:14 |
| Eccentricity: | 0.0202379 |
| inclination: | 66.6918° |
| perigee height: | 583 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 34.7661° |
| argument of perigee: | 90.7166° |
| revolutions per day: | 14.49478548 |
| mean anomaly at epoch: | 271.7134° |
| orbit number at epoch: | 21696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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