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 20442U 26037.99163419 +.00000000 +00000-0 +91526-4 0 00002
2 20442 98.8950 56.1487 0010841 224.2118 135.8201 14.34074785 01
| Epoch (UTC): | 06 February 2026 23:47:57 |
| Eccentricity: | 0.0010841 |
| inclination: | 98.8950° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 56.1487° |
| argument of perigee: | 224.2118° |
| revolutions per day: | 14.34074785 |
| mean anomaly at epoch: | 135.8201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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