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 23545U 26150.81781904 +.00000000 +00000-0 +73329-3 0 00001
2 23545 69.9614 283.4416 0003748 190.8928 169.2149 14.95708153 08
| Epoch (UTC): | 30 May 2026 19:37:39 |
| Eccentricity: | 0.0003748 |
| inclination: | 69.9614° |
| perigee height: | 578 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 283.4416° |
| argument of perigee: | 190.8928° |
| revolutions per day: | 14.95708153 |
| mean anomaly at epoch: | 169.2149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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