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 26905U 01040A 23307.78140934 0.00000350 00000-0 23783-3 0 05
2 26905 63.3897 188.7683 0573038 6.4533 353.5467 13.40992127 09
| Epoch (UTC): | 03 November 2023 18:45:13 |
| Eccentricity: | 0.0573038 |
| inclination: | 63.3897° |
| perigee height: | 677 km |
| apogee height: | 1534 km |
| right ascension of ascending node: | 188.7683° |
| argument of perigee: | 6.4533° |
| revolutions per day: | 13.40992127 |
| mean anomaly at epoch: | 353.5467° |
| 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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