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 23075.88766693 0.00000600 00000-0 42893-3 0 07
2 26907 63.3885 53.8436 0555541 5.5703 354.4297 13.41445588 00
| Epoch (UTC): | 16 March 2023 21:18:14 |
| Eccentricity: | 0.0555541 |
| inclination: | 63.3885° |
| perigee height: | 688 km |
| apogee height: | 1519 km |
| right ascension of ascending node: | 53.8436° |
| argument of perigee: | 5.5703° |
| revolutions per day: | 13.41445588 |
| mean anomaly at epoch: | 354.4297° |
| 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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