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 23343.06370010 .00000731 00000-0 15969-3 0 9999
2 00046 66.6885 213.2394 0212082 264.1594 93.5305 14.51172378323159
| Epoch (UTC): | 09 December 2023 01:31:43 |
| Eccentricity: | 0.0212082 |
| inclination: | 66.6885° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 213.2394° |
| argument of perigee: | 264.1594° |
| revolutions per day: | 14.51172378 |
| mean anomaly at epoch: | 93.5305° |
| orbit number at epoch: | 32315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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