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 00005U 26044.84585200 +.00000000 +00000-0 +13365-3 0 00007
2 00005 34.2592 334.9736 1838976 302.3178 41.2200 10.85948826 03
| Epoch (UTC): | 13 February 2026 20:18:01 |
| Eccentricity: | 0.1838976 |
| inclination: | 34.2592° |
| perigee height: | 652 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 334.9736° |
| argument of perigee: | 302.3178° |
| revolutions per day: | 10.85948826 |
| mean anomaly at epoch: | 41.2200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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