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 62833U 26145.47477920 +.00000000 +00000-0 +13266-2 0 00003
2 62833 43.0059 203.4546 0003602 284.5687 75.4782 15.70891680 08
| Epoch (UTC): | 25 May 2026 11:23:40 |
| Eccentricity: | 0.0003602 |
| inclination: | 43.0059° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 203.4546° |
| argument of perigee: | 284.5687° |
| revolutions per day: | 15.70891680 |
| mean anomaly at epoch: | 75.4782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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