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 62821U 26145.19558168 +.00000000 +00000-0 +59733-3 0 00003
2 62821 53.1581 314.0966 0001448 104.3509 255.7653 15.30204099 08
| Epoch (UTC): | 25 May 2026 04:41:38 |
| Eccentricity: | 0.0001448 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0966° |
| argument of perigee: | 104.3509° |
| revolutions per day: | 15.30204099 |
| mean anomaly at epoch: | 255.7653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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