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 21422U 26137.78197477 +.00000000 +00000-0 +57634-4 0 00002
2 21422 82.4981 17.0223 0012157 178.4770 181.6494 15.00349912 07
| Epoch (UTC): | 17 May 2026 18:46:02 |
| Eccentricity: | 0.0012157 |
| inclination: | 82.4981° |
| perigee height: | 557 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 17.0223° |
| argument of perigee: | 178.4770° |
| revolutions per day: | 15.00349912 |
| mean anomaly at epoch: | 181.6494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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