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 25197.92736230 .00001313 00000-0 11778-3 0 9995
2 22236 82.5058 144.6427 0012849 264.4041 95.5715 14.94968483745552
| Epoch (UTC): | 16 July 2025 22:15:24 |
| Eccentricity: | 0.0012849 |
| inclination: | 82.5058° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 144.6427° |
| argument of perigee: | 264.4041° |
| revolutions per day: | 14.94968483 |
| mean anomaly at epoch: | 95.5715° |
| orbit number at epoch: | 74555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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