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 17296U 87003B 25196.38208153 .00000346 00000-0 37328-4 0 9996
2 17296 82.5302 143.8149 0017433 204.1111 155.9291 14.85318513 80554
| Epoch (UTC): | 15 July 2025 09:10:11 |
| Eccentricity: | 0.0017433 |
| inclination: | 82.5302° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 143.8149° |
| argument of perigee: | 204.1111° |
| revolutions per day: | 14.85318513 |
| mean anomaly at epoch: | 155.9291° |
| orbit number at epoch: | 8055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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