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 is defined by the following mean orbital elements,
1 26907U 01040C 26010.72752581 0.00000700 00000-0 35153-3 0 05
2 26907 63.3740 281.7466 0645166 12.1775 347.9196 13.42260483 06
| Epoch (UTC): | 10 January 2026 17:27:38 |
| Eccentricity: | 0.0645166 |
| inclination: | 63.3740° |
| perigee height: | 618 km |
| apogee height: | 1583 km |
| right ascension of ascending node: | 281.7466° |
| argument of perigee: | 12.1775° |
| revolutions per day: | 13.42260483 |
| mean anomaly at epoch: | 347.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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