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 63159U 26145.58173623 +.00000000 +00000-0 +94096-4 0 00002
2 63159 88.9690 303.0371 0015202 18.0106 342.1580 13.51014536 01
| Epoch (UTC): | 25 May 2026 13:57:42 |
| Eccentricity: | 0.0015202 |
| inclination: | 88.9690° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 303.0371° |
| argument of perigee: | 18.0106° |
| revolutions per day: | 13.51014536 |
| mean anomaly at epoch: | 342.1580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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