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 51876U 26145.37928970 +.00000000 +00000-0 +79490-4 0 00006
2 51876 53.2143 24.8420 0001251 83.0548 277.0586 15.08836838 09
| Epoch (UTC): | 25 May 2026 09:06:10 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.8420° |
| argument of perigee: | 83.0548° |
| revolutions per day: | 15.08836838 |
| mean anomaly at epoch: | 277.0586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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