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 62494U 26145.57698162 +.00000000 +00000-0 +58468-3 0 00004
2 62494 42.9983 214.4802 0000311 50.0567 310.0312 15.27588764 04
| Epoch (UTC): | 25 May 2026 13:50:51 |
| Eccentricity: | 0.0000311 |
| inclination: | 42.9983° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 214.4802° |
| argument of perigee: | 50.0567° |
| revolutions per day: | 15.27588764 |
| mean anomaly at epoch: | 310.0312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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