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 63044U 26145.35315194 +.00000000 +00000-0 +13503-2 0 00003
2 63044 53.1601 274.1561 0000677 36.5701 323.5347 15.34410147 00
| Epoch (UTC): | 25 May 2026 08:28:32 |
| Eccentricity: | 0.0000677 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 274.1561° |
| argument of perigee: | 36.5701° |
| revolutions per day: | 15.34410147 |
| mean anomaly at epoch: | 323.5347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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