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 51735U 26145.49797170 +.00000000 +00000-0 +98836-4 0 00004
2 51735 53.2118 334.3159 0001364 93.8406 266.2742 15.08831686 00
| Epoch (UTC): | 25 May 2026 11:57:04 |
| Eccentricity: | 0.0001364 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.3159° |
| argument of perigee: | 93.8406° |
| revolutions per day: | 15.08831686 |
| mean anomaly at epoch: | 266.2742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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