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 210U 61015BE 24358.12512269 .00001084 00000-0 96163-3 0 9997
2 210 66.4568 260.2187 0051965 291.5934 67.9608 13.88190132190670
| Epoch (UTC): | 23 December 2024 03:00:10 |
| Eccentricity: | 0.0051965 |
| inclination: | 66.4568° |
| perigee height: | 897 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 260.2187° |
| argument of perigee: | 291.5934° |
| revolutions per day: | 13.88190132 |
| mean anomaly at epoch: | 67.9608° |
| orbit number at epoch: | 19067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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