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 43623U 26142.62739226 +.00000000 +00000-0 +00000-0 0 00003
2 43623 56.6051 63.4972 0006625 351.7889 8.1977 1.86231107 05
| Epoch (UTC): | 22 May 2026 15:03:26 |
| Eccentricity: | 0.0006625 |
| inclination: | 56.6051° |
| perigee height: | 21510 km |
| apogee height: | 21547 km |
| right ascension of ascending node: | 63.4972° |
| argument of perigee: | 351.7889° |
| revolutions per day: | 1.86231107 |
| mean anomaly at epoch: | 8.1977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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