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 61529U 26145.37197326 +.00000000 +00000-0 +21339-4 0 00004
2 61529 53.1596 143.3792 0001025 88.8440 271.2679 15.30194476 07
| Epoch (UTC): | 25 May 2026 08:55:38 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.3792° |
| argument of perigee: | 88.8440° |
| revolutions per day: | 15.30194476 |
| mean anomaly at epoch: | 271.2679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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