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 26088.17537505 +.00000000 +00000-0 +19680-3 0 00003
2 23317 82.5350 331.4122 0016152 177.9435 182.1857 14.96967191 03
| Epoch (UTC): | 29 March 2026 04:12:32 |
| Eccentricity: | 0.0016152 |
| inclination: | 82.5350° |
| perigee height: | 565 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 331.4122° |
| argument of perigee: | 177.9435° |
| revolutions per day: | 14.96967191 |
| mean anomaly at epoch: | 182.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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