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 00463U 61015EZ 24357.32854466 .00006379 00000-0 15557-2 0 9995
2 00463 66.7689 81.3295 0051940 306.9524 52.6835 14.52443982290285
| Epoch (UTC): | 22 December 2024 07:53:06 |
| Eccentricity: | 0.0051940 |
| inclination: | 66.7689° |
| perigee height: | 681 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 81.3295° |
| argument of perigee: | 306.9524° |
| revolutions per day: | 14.52443982 |
| mean anomaly at epoch: | 52.6835° |
| orbit number at epoch: | 29028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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