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 22237U 26109.10460985 +.00000000 +00000-0 +27971-4 0 00000
2 22237 82.5134 352.5396 0020542 82.4945 277.8601 14.80344837 02
| Epoch (UTC): | 19 April 2026 02:30:38 |
| Eccentricity: | 0.0020542 |
| inclination: | 82.5134° |
| perigee height: | 614 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 352.5396° |
| argument of perigee: | 82.4945° |
| revolutions per day: | 14.80344837 |
| mean anomaly at epoch: | 277.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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