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 14552U 83122B 25198.49421395 .00000330 00000-0 35276-4 0 9998
2 14552 82.5225 190.6618 0017802 133.9849 226.2838 14.85548468225912
| Epoch (UTC): | 17 July 2025 11:51:40 |
| Eccentricity: | 0.0017802 |
| inclination: | 82.5225° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 190.6618° |
| argument of perigee: | 133.9849° |
| revolutions per day: | 14.85548468 |
| mean anomaly at epoch: | 226.2838° |
| orbit number at epoch: | 22591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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