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 17192U 86097B 25191.61406586 .00000312 00000-0 33197-4 0 9997
2 17192 82.5057 10.1573 0017811 104.4231 322.8790 14.85600596 64408
| Epoch (UTC): | 10 July 2025 14:44:15 |
| Eccentricity: | 0.0017811 |
| inclination: | 82.5057° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 10.1573° |
| argument of perigee: | 104.4231° |
| revolutions per day: | 14.85600596 |
| mean anomaly at epoch: | 322.8790° |
| orbit number at epoch: | 6440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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