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 26474U 26064.98605308 +.00000000 +00000-0 +30594-3 0 00007
2 26474 67.9892 50.9239 0038249 39.7616 320.6325 15.09517041 06
| Epoch (UTC): | 05 March 2026 23:39:54 |
| Eccentricity: | 0.0038249 |
| inclination: | 67.9892° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 50.9239° |
| argument of perigee: | 39.7616° |
| revolutions per day: | 15.09517041 |
| mean anomaly at epoch: | 320.6325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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