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 26019.31331428 +.00000000 +00000-0 +14284-3 0 00007
2 00045 66.6936 33.9647 0256393 267.9407 89.2317 14.35831160 04
| Epoch (UTC): | 19 January 2026 07:31:10 |
| Eccentricity: | 0.0256393 |
| inclination: | 66.6936° |
| perigee height: | 589 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 33.9647° |
| argument of perigee: | 267.9407° |
| revolutions per day: | 14.35831160 |
| mean anomaly at epoch: | 89.2317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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