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 27432U 02024C 25198.17305681 .00000012 00000-0 29625-4 0 9993
2 27432 98.9215 247.2614 0049637 332.6588 94.1945 14.14491286195944
| Epoch (UTC): | 17 July 2025 04:09:12 |
| Eccentricity: | 0.0049637 |
| inclination: | 98.9215° |
| perigee height: | 808 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 247.2614° |
| argument of perigee: | 332.6588° |
| revolutions per day: | 14.14491286 |
| mean anomaly at epoch: | 94.1945° |
| orbit number at epoch: | 19594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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