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 62142U 26145.19632258 +.00000000 +00000-0 +64624-3 0 00007
2 62142 43.0004 93.5622 0001245 266.6656 93.4053 15.27588348 09
| Epoch (UTC): | 25 May 2026 04:42:42 |
| Eccentricity: | 0.0001245 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.5622° |
| argument of perigee: | 266.6656° |
| revolutions per day: | 15.27588348 |
| mean anomaly at epoch: | 93.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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