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 data is extracted from the following two-line orbital elements,
1 22236U 92080A 25194.37991403 .00001321 00000-0 11849-3 0 9994
2 22236 82.5056 148.0322 0012912 278.0039 81.9717 14.94959164766078
| Epoch (UTC): | 13 July 2025 09:07:04 |
| Eccentricity: | 0.0012912 |
| inclination: | 82.5056° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 148.0322° |
| argument of perigee: | 278.0039° |
| revolutions per day: | 14.94959164 |
| mean anomaly at epoch: | 81.9717° |
| orbit number at epoch: | 76607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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