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 51755U 26145.20081015 +.00000000 +00000-0 +14073-4 0 00000
2 51755 53.2137 325.6498 0001272 93.5650 266.5488 15.08835389 02
| Epoch (UTC): | 25 May 2026 04:49:09 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 325.6498° |
| argument of perigee: | 93.5650° |
| revolutions per day: | 15.08835389 |
| mean anomaly at epoch: | 266.5488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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