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 26053.82963047 +.00000000 +00000-0 +62803-4 0 00003
2 20442 98.8946 72.4355 0011638 176.3243 183.8028 14.34081031 04
| Epoch (UTC): | 22 February 2026 19:54:40 |
| Eccentricity: | 0.0011638 |
| inclination: | 98.8946° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 72.4355° |
| argument of perigee: | 176.3243° |
| revolutions per day: | 14.34081031 |
| mean anomaly at epoch: | 183.8028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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