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 63091U 26145.44688088 +.00000000 +00000-0 +27492-3 0 00003
2 63091 70.0006 160.7569 0004373 265.4876 94.5784 14.98337568 04
| Epoch (UTC): | 25 May 2026 10:43:30 |
| Eccentricity: | 0.0004373 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.7569° |
| argument of perigee: | 265.4876° |
| revolutions per day: | 14.98337568 |
| mean anomaly at epoch: | 94.5784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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