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 26546U 26106.75840178 +.00000000 +00000-0 +13649-3 0 00007
2 26546 64.5482 265.9037 0039782 290.3501 69.3344 15.05142512 00
| Epoch (UTC): | 16 April 2026 18:12:05 |
| Eccentricity: | 0.0039782 |
| inclination: | 64.5482° |
| perigee height: | 524 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 265.9037° |
| argument of perigee: | 290.3501° |
| revolutions per day: | 15.05142512 |
| mean anomaly at epoch: | 69.3344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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