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 67877U 26145.45867125 +.00000000 +00000-0 +47800-3 0 00006
2 67877 53.1575 208.0829 0001051 87.0775 273.0346 15.29376243 00
| Epoch (UTC): | 25 May 2026 11:00:29 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.1575° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 208.0829° |
| argument of perigee: | 87.0775° |
| revolutions per day: | 15.29376243 |
| mean anomaly at epoch: | 273.0346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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