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 56317U 26144.96086088 +.00000000 +00000-0 -59475-4 0 00002
2 56317 97.4530 146.0363 0001590 84.0828 276.0580 15.05674629 03
| Epoch (UTC): | 24 May 2026 23:03:38 |
| Eccentricity: | 0.0001590 |
| inclination: | 97.4530° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.0363° |
| argument of perigee: | 84.0828° |
| revolutions per day: | 15.05674629 |
| mean anomaly at epoch: | 276.0580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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