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 63460U 26145.58710183 +.00000000 +00000-0 +71309-3 0 00006
2 63460 42.9998 185.8390 0001724 273.9499 86.1156 15.27586522 03
| Epoch (UTC): | 25 May 2026 14:05:25 |
| Eccentricity: | 0.0001724 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8390° |
| argument of perigee: | 273.9499° |
| revolutions per day: | 15.27586522 |
| mean anomaly at epoch: | 86.1156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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