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 23317U 26142.11457735 +.00000000 +00000-0 +10598-3 0 00003
2 23317 82.5325 279.8744 0016276 7.0725 353.0723 14.97145434 02
| Epoch (UTC): | 22 May 2026 02:44:59 |
| Eccentricity: | 0.0016276 |
| inclination: | 82.5325° |
| perigee height: | 564 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 279.8744° |
| argument of perigee: | 7.0725° |
| revolutions per day: | 14.97145434 |
| mean anomaly at epoch: | 353.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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