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 61957U 26145.31085289 +.00000000 +00000-0 +26070-1 0 00001
2 61957 53.1583 143.9675 0017757 265.0929 94.8051 15.45573474 02
| Epoch (UTC): | 25 May 2026 07:27:37 |
| Eccentricity: | 0.0017757 |
| inclination: | 53.1583° |
| perigee height: | 418 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 143.9675° |
| argument of perigee: | 265.0929° |
| revolutions per day: | 15.45573474 |
| mean anomaly at epoch: | 94.8051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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