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 63717U 26145.51715014 +.00000000 +00000-0 +44438-3 0 00005
2 63717 53.1595 222.5940 0001552 74.0043 286.1129 15.30209186 03
| Epoch (UTC): | 25 May 2026 12:24:41 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.5940° |
| argument of perigee: | 74.0043° |
| revolutions per day: | 15.30209186 |
| mean anomaly at epoch: | 286.1129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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