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 65720U 26145.46408804 +.00000000 +00000-0 +19862-3 0 00004
2 65720 49.9923 53.6923 0009455 125.9725 234.2091 14.83268576 01
| Epoch (UTC): | 25 May 2026 11:08:17 |
| Eccentricity: | 0.0009455 |
| inclination: | 49.9923° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 53.6923° |
| argument of perigee: | 125.9725° |
| revolutions per day: | 14.83268576 |
| mean anomaly at epoch: | 234.2091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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