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 62611U 26145.17767689 +.00000000 +00000-0 +27725-3 0 00004
2 62611 97.3921 224.7063 0008319 64.4294 295.7803 15.24673639 03
| Epoch (UTC): | 25 May 2026 04:15:51 |
| Eccentricity: | 0.0008319 |
| inclination: | 97.3921° |
| perigee height: | 486 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 224.7063° |
| argument of perigee: | 64.4294° |
| revolutions per day: | 15.24673639 |
| mean anomaly at epoch: | 295.7803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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