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 62485U 26145.75169875 +.00000000 +00000-0 +00000-0 0 00004
2 62485 5.0620 61.3084 0051796 171.4431 48.6039 1.00267548 04
| Epoch (UTC): | 25 May 2026 18:02:26 |
| Eccentricity: | 0.0051796 |
| inclination: | 5.0620° |
| perigee height: | 35569 km |
| apogee height: | 36006 km |
| right ascension of ascending node: | 61.3084° |
| argument of perigee: | 171.4431° |
| revolutions per day: | 1.00267548 |
| mean anomaly at epoch: | 48.6039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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