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 is defined by the following mean orbital elements,
1 17240U 26088.23366101 +.00000000 +00000-0 +61475-4 0 00000
2 17240 82.9355 192.3337 0028231 287.1540 134.3409 13.74283642 03
| Epoch (UTC): | 29 March 2026 05:36:28 |
| Eccentricity: | 0.0028231 |
| inclination: | 82.9355° |
| perigee height: | 963 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 192.3337° |
| argument of perigee: | 287.1540° |
| revolutions per day: | 13.74283642 |
| mean anomaly at epoch: | 134.3409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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