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 61589U 26145.12465491 +.00000000 +00000-0 +87817-4 0 00007
2 61589 53.1613 54.5418 0001140 122.6990 237.4121 15.30218384 07
| Epoch (UTC): | 25 May 2026 02:59:30 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.5418° |
| argument of perigee: | 122.6990° |
| revolutions per day: | 15.30218384 |
| mean anomaly at epoch: | 237.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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