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 42664U 61028K 25207.28853254 .00000004 00000-0 29512-2 0 9997
2 42664 95.8256 168.3405 0344171 185.2262 174.4948 8.69044360322141
| Epoch (UTC): | 26 July 2025 06:55:29 |
| Eccentricity: | 0.0344171 |
| inclination: | 95.8256° |
| perigee height: | 3271 km |
| apogee height: | 3959 km |
| right ascension of ascending node: | 168.3405° |
| argument of perigee: | 185.2262° |
| revolutions per day: | 8.69044360 |
| mean anomaly at epoch: | 174.4948° |
| orbit number at epoch: | 32214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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