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 56915U 26145.61701924 +.00000000 +00000-0 +31394-4 0 00001
2 56915 43.0020 356.2018 0001020 265.2283 94.8453 15.27572860 09
| Epoch (UTC): | 25 May 2026 14:48:30 |
| Eccentricity: | 0.0001020 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2018° |
| argument of perigee: | 265.2283° |
| revolutions per day: | 15.27572860 |
| mean anomaly at epoch: | 94.8453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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