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 51152U 26145.47308742 +.00000000 +00000-0 +11446-4 0 00000
2 51152 53.2146 324.0420 0001456 92.3879 267.7280 15.08832924 00
| Epoch (UTC): | 25 May 2026 11:21:14 |
| Eccentricity: | 0.0001456 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.0420° |
| argument of perigee: | 92.3879° |
| revolutions per day: | 15.08832924 |
| mean anomaly at epoch: | 267.7280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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