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 63599U 26145.61483272 +.00000000 +00000-0 +60503-4 0 00004
2 63599 99.6900 153.1827 0001233 88.7937 271.3342 13.57247789 00
| Epoch (UTC): | 25 May 2026 14:45:21 |
| Eccentricity: | 0.0001233 |
| inclination: | 99.6900° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.1827° |
| argument of perigee: | 88.7937° |
| revolutions per day: | 13.57247789 |
| mean anomaly at epoch: | 271.3342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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