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 26907U 01040C 23271.11807155 0.00000299 00000-0 19853-3 0 04
2 26907 63.3914 272.4225 0576340 6.5224 353.5190 13.41522918 02
| Epoch (UTC): | 28 September 2023 02:50:01 |
| Eccentricity: | 0.0576340 |
| inclination: | 63.3914° |
| perigee height: | 672 km |
| apogee height: | 1535 km |
| right ascension of ascending node: | 272.4225° |
| argument of perigee: | 6.5224° |
| revolutions per day: | 13.41522918 |
| mean anomaly at epoch: | 353.5190° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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