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 63762U 26145.57773028 +.00000000 +00000-0 +13996-2 0 00004
2 63762 42.9992 189.1740 0000261 322.4430 37.6419 15.70881203 03
| Epoch (UTC): | 25 May 2026 13:51:55 |
| Eccentricity: | 0.0000261 |
| inclination: | 42.9992° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 189.1740° |
| argument of perigee: | 322.4430° |
| revolutions per day: | 15.70881203 |
| mean anomaly at epoch: | 37.6419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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