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 20624U 26109.25210507 +.00000000 +00000-0 +68569-4 0 00005
2 20624 71.0400 295.7152 0013653 149.4986 210.6933 14.14840283 07
| Epoch (UTC): | 19 April 2026 06:03:01 |
| Eccentricity: | 0.0013653 |
| inclination: | 71.0400° |
| perigee height: | 833 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 295.7152° |
| argument of perigee: | 149.4986° |
| revolutions per day: | 14.14840283 |
| mean anomaly at epoch: | 210.6933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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