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 63363U 26145.45968338 +.00000000 +00000-0 +57878-3 0 00006
2 63363 53.1615 53.0222 0001432 80.9296 279.1867 15.30213723 09
| Epoch (UTC): | 25 May 2026 11:01:56 |
| Eccentricity: | 0.0001432 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.0222° |
| argument of perigee: | 80.9296° |
| revolutions per day: | 15.30213723 |
| mean anomaly at epoch: | 279.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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