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 63033U 26145.34080887 +.00000000 +00000-0 +76832-3 0 00003
2 63033 53.1590 262.0047 0001258 82.4561 277.6583 15.30214095 01
| Epoch (UTC): | 25 May 2026 08:10:45 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.0047° |
| argument of perigee: | 82.4561° |
| revolutions per day: | 15.30214095 |
| mean anomaly at epoch: | 277.6583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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