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 62141U 26145.52793972 +.00000000 +00000-0 +12113-2 0 00009
2 62141 42.9999 83.9748 0001419 266.2252 93.8437 15.27610436 06
| Epoch (UTC): | 25 May 2026 12:40:13 |
| Eccentricity: | 0.0001419 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.9748° |
| argument of perigee: | 266.2252° |
| revolutions per day: | 15.27610436 |
| mean anomaly at epoch: | 93.8437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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