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 56121U 26145.16521485 +.00000000 +00000-0 +96556-5 0 00004
2 56121 43.0015 75.3065 0000839 243.6826 116.3939 15.27575690 06
| Epoch (UTC): | 25 May 2026 03:57:54 |
| Eccentricity: | 0.0000839 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.3065° |
| argument of perigee: | 243.6826° |
| revolutions per day: | 15.27575690 |
| mean anomaly at epoch: | 116.3939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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