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 51750U 26145.47409065 +.00000000 +00000-0 +22952-4 0 00008
2 51750 53.2146 324.4329 0001500 90.3544 269.7620 15.08835238 04
| Epoch (UTC): | 25 May 2026 11:22:41 |
| Eccentricity: | 0.0001500 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.4329° |
| argument of perigee: | 90.3544° |
| revolutions per day: | 15.08835238 |
| mean anomaly at epoch: | 269.7620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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