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 61679U 26145.25032779 +.00000000 +00000-0 +11335-3 0 00001
2 61679 53.1608 95.7239 0001446 94.6858 265.4308 15.30173155 03
| Epoch (UTC): | 25 May 2026 06:00:28 |
| Eccentricity: | 0.0001446 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.7239° |
| argument of perigee: | 94.6858° |
| revolutions per day: | 15.30173155 |
| mean anomaly at epoch: | 265.4308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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