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 26074.80639328 +.00000000 +00000-0 +16505-3 0 00007
2 23317 82.5375 344.1763 0015007 224.6525 135.3490 14.96913194 07
| Epoch (UTC): | 15 March 2026 19:21:12 |
| Eccentricity: | 0.0015007 |
| inclination: | 82.5375° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 344.1763° |
| argument of perigee: | 224.6525° |
| revolutions per day: | 14.96913194 |
| mean anomaly at epoch: | 135.3490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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