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 21423U 26017.97756620 +.00000000 +00000-0 +42705-4 0 00005
2 21423 82.4926 267.7461 0018269 50.9529 309.3307 14.81776172 03
| Epoch (UTC): | 17 January 2026 23:27:41 |
| Eccentricity: | 0.0018269 |
| inclination: | 82.4926° |
| perigee height: | 611 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 267.7461° |
| argument of perigee: | 50.9529° |
| revolutions per day: | 14.81776172 |
| mean anomaly at epoch: | 309.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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