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 23089.63736929 .00001895 00000-0 39744-3 0 9993
2 00046 66.6904 179.5701 0199630 93.3616 269.0349 14.50336600286398
| Epoch (UTC): | 30 March 2023 15:17:48 |
| Eccentricity: | 0.0199630 |
| inclination: | 66.6904° |
| perigee height: | 583 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 179.5701° |
| argument of perigee: | 93.3616° |
| revolutions per day: | 14.50336600 |
| mean anomaly at epoch: | 269.0349° |
| orbit number at epoch: | 28639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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