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 61779U 26145.58295257 +.00000000 +00000-0 +26604-3 0 00005
2 61779 97.3064 15.0872 0013760 35.0446 325.1701 15.36551763 04
| Epoch (UTC): | 25 May 2026 13:59:27 |
| Eccentricity: | 0.0013760 |
| inclination: | 97.3064° |
| perigee height: | 447 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 15.0872° |
| argument of perigee: | 35.0446° |
| revolutions per day: | 15.36551763 |
| mean anomaly at epoch: | 325.1701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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