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 23028.87757046 .00000603 00000-0 14179-3 0 9996
2 00046 66.6916 343.9620 0203229 140.2548 221.3655 14.50067040277585
| Epoch (UTC): | 28 January 2023 21:03:42 |
| Eccentricity: | 0.0203229 |
| inclination: | 66.6916° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 343.9620° |
| argument of perigee: | 140.2548° |
| revolutions per day: | 14.50067040 |
| mean anomaly at epoch: | 221.3655° |
| orbit number at epoch: | 27758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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