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 63710U 26145.59366872 +.00000000 +00000-0 -28503-3 0 00006
2 63710 53.1596 222.3697 0000840 61.0331 299.0755 15.31699163 06
| Epoch (UTC): | 25 May 2026 14:14:52 |
| Eccentricity: | 0.0000840 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.3697° |
| argument of perigee: | 61.0331° |
| revolutions per day: | 15.31699163 |
| mean anomaly at epoch: | 299.0755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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