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 61526U 26145.27786037 +.00000000 +00000-0 +52323-4 0 00000
2 61526 53.1594 147.0309 0001234 78.8476 281.2663 15.30196932 00
| Epoch (UTC): | 25 May 2026 06:40:07 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 147.0309° |
| argument of perigee: | 78.8476° |
| revolutions per day: | 15.30196932 |
| mean anomaly at epoch: | 281.2663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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