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 26073.78400388 +.00000000 +00000-0 +84803-4 0 00008
2 20442 98.8932 92.9553 0012531 120.6273 239.6149 14.34090436 07
| Epoch (UTC): | 14 March 2026 18:48:57 |
| Eccentricity: | 0.0012531 |
| inclination: | 98.8932° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 92.9553° |
| argument of perigee: | 120.6273° |
| revolutions per day: | 14.34090436 |
| mean anomaly at epoch: | 239.6149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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