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 63024U 26145.39541275 +.00000000 +00000-0 +43734-3 0 00006
2 63024 43.0004 262.6401 0001587 274.4965 85.5705 15.27596655 08
| Epoch (UTC): | 25 May 2026 09:29:23 |
| Eccentricity: | 0.0001587 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.6401° |
| argument of perigee: | 274.4965° |
| revolutions per day: | 15.27596655 |
| mean anomaly at epoch: | 85.5705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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