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 63687U 26145.58691787 +.00000000 +00000-0 +15337-3 0 00004
2 63687 86.5033 320.7492 0001443 82.5812 277.5486 13.24409087 09
| Epoch (UTC): | 25 May 2026 14:05:09 |
| Eccentricity: | 0.0001443 |
| inclination: | 86.5033° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.7492° |
| argument of perigee: | 82.5812° |
| revolutions per day: | 13.24409087 |
| mean anomaly at epoch: | 277.5486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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