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 65714U 26145.14972582 +.00000000 +00000-0 +21838-3 0 00007
2 65714 49.9855 55.2471 0009948 124.4560 235.7319 14.83265492 05
| Epoch (UTC): | 25 May 2026 03:35:36 |
| Eccentricity: | 0.0009948 |
| inclination: | 49.9855° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 55.2471° |
| argument of perigee: | 124.4560° |
| revolutions per day: | 14.83265492 |
| mean anomaly at epoch: | 235.7319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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