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 17997U 26146.27742882 +.00000000 +00000-0 +93532-3 0 00000
2 17997 63.2931 259.2268 0682472 107.6615 260.0123 14.12290683 08
| Epoch (UTC): | 26 May 2026 06:39:29 |
| Eccentricity: | 0.0682472 |
| inclination: | 63.2931° |
| perigee height: | 358 km |
| apogee height: | 1345 km |
| right ascension of ascending node: | 259.2268° |
| argument of perigee: | 107.6615° |
| revolutions per day: | 14.12290683 |
| mean anomaly at epoch: | 260.0123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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