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 62283U 26145.42463850 +.00000000 +00000-0 +52788-3 0 00007
2 62283 43.0019 132.0892 0001454 265.7754 94.2932 15.27593192 08
| Epoch (UTC): | 25 May 2026 10:11:28 |
| Eccentricity: | 0.0001454 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.0892° |
| argument of perigee: | 265.7754° |
| revolutions per day: | 15.27593192 |
| mean anomaly at epoch: | 94.2932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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