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 22889U 93070B 25197.76079826 .00000057 00000-0 41813-4 0 9990
2 22889 82.9458 281.2255 0048644 233.2522 126.4165 13.78229520593873
| Epoch (UTC): | 16 July 2025 18:15:32 |
| Eccentricity: | 0.0048644 |
| inclination: | 82.9458° |
| perigee height: | 934 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 281.2255° |
| argument of perigee: | 233.2522° |
| revolutions per day: | 13.78229520 |
| mean anomaly at epoch: | 126.4165° |
| orbit number at epoch: | 59387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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