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 25188.89136887 .00001377 00000-0 12364-3 0 9995
2 22236 82.5051 153.2763 0013073 298.5690 61.4215 14.94944427744202
| Epoch (UTC): | 07 July 2025 21:23:34 |
| Eccentricity: | 0.0013073 |
| inclination: | 82.5051° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 153.2763° |
| argument of perigee: | 298.5690° |
| revolutions per day: | 14.94944427 |
| mean anomaly at epoch: | 61.4215° |
| orbit number at epoch: | 74420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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