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 62921U 26145.46620157 +.00000000 +00000-0 +93732-3 0 00009
2 62921 43.0045 55.3286 0001538 258.0593 102.0087 15.27585322 04
| Epoch (UTC): | 25 May 2026 11:11:19 |
| Eccentricity: | 0.0001538 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.3286° |
| argument of perigee: | 258.0593° |
| revolutions per day: | 15.27585322 |
| mean anomaly at epoch: | 102.0087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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