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 56527U 26145.43093153 +.00000000 +00000-0 +11967-4 0 00002
2 56527 43.0013 142.7038 0000988 276.5656 83.5083 15.27578299 07
| Epoch (UTC): | 25 May 2026 10:20:32 |
| Eccentricity: | 0.0000988 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.7038° |
| argument of perigee: | 276.5656° |
| revolutions per day: | 15.27578299 |
| mean anomaly at epoch: | 83.5083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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