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 62018U 26145.08303538 +.00000000 +00000-0 +15553-2 0 00009
2 62018 53.1578 24.6714 0000846 75.9688 284.1424 15.69774482 01
| Epoch (UTC): | 25 May 2026 01:59:34 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1578° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 24.6714° |
| argument of perigee: | 75.9688° |
| revolutions per day: | 15.69774482 |
| mean anomaly at epoch: | 284.1424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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