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 00045U 26044.94630808 +.00000000 +00000-0 +88534-4 0 00008
2 00045 66.6950 326.1695 0255651 249.7507 107.5945 14.35869755 07
| Epoch (UTC): | 13 February 2026 22:42:41 |
| Eccentricity: | 0.0255651 |
| inclination: | 66.6950° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 326.1695° |
| argument of perigee: | 249.7507° |
| revolutions per day: | 14.35869755 |
| mean anomaly at epoch: | 107.5945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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