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 22236U 26038.80867536 +.00000000 +00000-0 +25301-3 0 00004
2 22236 82.5057 307.6981 0012962 297.2556 62.7345 14.96081385 06
| Epoch (UTC): | 07 February 2026 19:24:29 |
| Eccentricity: | 0.0012962 |
| inclination: | 82.5057° |
| perigee height: | 570 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 307.6981° |
| argument of perigee: | 297.2556° |
| revolutions per day: | 14.96081385 |
| mean anomaly at epoch: | 62.7345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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