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 62158U 26145.54335196 +.00000000 +00000-0 +52961-3 0 00005
2 62158 42.9995 84.0868 0000498 324.2542 35.8276 15.27587697 07
| Epoch (UTC): | 25 May 2026 13:02:25 |
| Eccentricity: | 0.0000498 |
| inclination: | 42.9995° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 84.0868° |
| argument of perigee: | 324.2542° |
| revolutions per day: | 15.27587697 |
| mean anomaly at epoch: | 35.8276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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