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 26906U 01040B 25348.20191830 .00000640 00000-0 39761-3 0 9993
2 26906 63.4236 275.4895 0612421 341.2910 16.6457 13.45100108 78529
| Epoch (UTC): | 14 December 2025 04:50:45 |
| Eccentricity: | 0.0612421 |
| inclination: | 63.4236° |
| perigee height: | 633 km |
| apogee height: | 1548 km |
| right ascension of ascending node: | 275.4895° |
| argument of perigee: | 341.2910° |
| revolutions per day: | 13.45100108 |
| mean anomaly at epoch: | 16.6457° |
| orbit number at epoch: | 7852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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