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 25198.33573617 .00000376 00000-0 40900-4 0 9996
2 17296 82.5304 141.9822 0017600 197.4487 162.6127 14.85320011 59767
| Epoch (UTC): | 17 July 2025 08:03:27 |
| Eccentricity: | 0.0017600 |
| inclination: | 82.5304° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 141.9822° |
| argument of perigee: | 197.4487° |
| revolutions per day: | 14.85320011 |
| mean anomaly at epoch: | 162.6127° |
| orbit number at epoch: | 5976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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