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 20437U 26053.72584838 +.00000000 +00000-0 +46064-4 0 00004
2 20437 98.8203 100.9979 0009523 236.4769 237.0826 14.33234938 07
| Epoch (UTC): | 22 February 2026 17:25:13 |
| Eccentricity: | 0.0009523 |
| inclination: | 98.8203° |
| perigee height: | 774 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 100.9979° |
| argument of perigee: | 236.4769° |
| revolutions per day: | 14.33234938 |
| mean anomaly at epoch: | 237.0826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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