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 23332.17428299 .00002259 00000-0 44606-3 0 9999
2 00046 66.6907 242.7524 0212274 271.9998 85.6815 14.51133596321574
| Epoch (UTC): | 28 November 2023 04:10:58 |
| Eccentricity: | 0.0212274 |
| inclination: | 66.6907° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 242.7524° |
| argument of perigee: | 271.9998° |
| revolutions per day: | 14.51133596 |
| mean anomaly at epoch: | 85.6815° |
| orbit number at epoch: | 32157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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