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 56877U 26145.31770454 +.00000000 +00000-0 +17730-4 0 00007
2 56877 43.0031 12.0992 0001115 237.6773 122.3971 15.27579333 02
| Epoch (UTC): | 25 May 2026 07:37:29 |
| Eccentricity: | 0.0001115 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.0992° |
| argument of perigee: | 237.6773° |
| revolutions per day: | 15.27579333 |
| mean anomaly at epoch: | 122.3971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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