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 63686U 26145.49259259 +.00000000 +00000-0 +53686-3 0 00006
2 63686 42.9972 317.3725 0000813 283.7718 76.3043 15.27592757 03
| Epoch (UTC): | 25 May 2026 11:49:20 |
| Eccentricity: | 0.0000813 |
| inclination: | 42.9972° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.3725° |
| argument of perigee: | 283.7718° |
| revolutions per day: | 15.27592757 |
| mean anomaly at epoch: | 76.3043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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