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 51129U 26145.20268597 +.00000000 +00000-0 -21966-4 0 00007
2 51129 53.2141 315.6397 0001177 92.6116 267.5011 15.08837836 02
| Epoch (UTC): | 25 May 2026 04:51:52 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 315.6397° |
| argument of perigee: | 92.6116° |
| revolutions per day: | 15.08837836 |
| mean anomaly at epoch: | 267.5011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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