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 26155.08104029 +.00000000 +00000-0 +58711-4 0 00008
2 20437 98.8034 204.1265 0009424 306.1446 112.5053 14.33264245 04
| Epoch (UTC): | 04 June 2026 01:56:41 |
| Eccentricity: | 0.0009424 |
| inclination: | 98.8034° |
| perigee height: | 774 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 204.1265° |
| argument of perigee: | 306.1446° |
| revolutions per day: | 14.33264245 |
| mean anomaly at epoch: | 112.5053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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