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 56558U 26145.46547061 +.00000000 +00000-0 +13373-4 0 00004
2 56558 43.0028 153.4248 0001165 302.7567 57.3172 15.27577315 06
| Epoch (UTC): | 25 May 2026 11:10:16 |
| Eccentricity: | 0.0001165 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.4248° |
| argument of perigee: | 302.7567° |
| revolutions per day: | 15.27577315 |
| mean anomaly at epoch: | 57.3172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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