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 25188.90428696 .00000350 00000-0 37898-4 0 9998
2 17296 82.5295 150.8299 0016892 230.1776 129.7954 14.85313708 58363
| Epoch (UTC): | 07 July 2025 21:42:10 |
| Eccentricity: | 0.0016892 |
| inclination: | 82.5295° |
| perigee height: | 601 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 150.8299° |
| argument of perigee: | 230.1776° |
| revolutions per day: | 14.85313708 |
| mean anomaly at epoch: | 129.7954° |
| orbit number at epoch: | 5836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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