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 62474U 26144.93713652 +.00000000 +00000-0 +18087-2 0 00005
2 62474 42.9995 123.3244 0001163 212.3277 147.7520 15.70958313 05
| Epoch (UTC): | 24 May 2026 22:29:28 |
| Eccentricity: | 0.0001163 |
| inclination: | 42.9995° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 123.3244° |
| argument of perigee: | 212.3277° |
| revolutions per day: | 15.70958313 |
| mean anomaly at epoch: | 147.7520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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