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 62879U 26145.18235154 +.00000000 +00000-0 +16583-2 0 00007
2 62879 43.0007 80.6776 0001464 266.3551 93.7149 15.70902964 01
| Epoch (UTC): | 25 May 2026 04:22:35 |
| Eccentricity: | 0.0001464 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 80.6776° |
| argument of perigee: | 266.3551° |
| revolutions per day: | 15.70902964 |
| mean anomaly at epoch: | 93.7149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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