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 26931U 01043C 24357.86388229 .00000407 00000-0 18404-3 0 9997
2 26931 67.0492 204.0023 0006560 260.3339 99.7022 14.31548009212958
| Epoch (UTC): | 22 December 2024 20:43:59 |
| Eccentricity: | 0.0006560 |
| inclination: | 67.0492° |
| perigee height: | 782 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 204.0023° |
| argument of perigee: | 260.3339° |
| revolutions per day: | 14.31548009 |
| mean anomaly at epoch: | 99.7022° |
| orbit number at epoch: | 21295 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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