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 63178U 26145.48332299 +.00000000 +00000-0 +74351-4 0 00000
2 63178 97.9565 331.3569 0010017 226.5559 133.4818 14.74740901 06
| Epoch (UTC): | 25 May 2026 11:35:59 |
| Eccentricity: | 0.0010017 |
| inclination: | 97.9565° |
| perigee height: | 639 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 331.3569° |
| argument of perigee: | 226.5559° |
| revolutions per day: | 14.74740901 |
| mean anomaly at epoch: | 133.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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