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 61523U 26145.38527904 +.00000000 +00000-0 +16129-4 0 00009
2 61523 53.1601 146.2847 0001196 85.2378 274.8759 15.30189630 05
| Epoch (UTC): | 25 May 2026 09:14:48 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.2847° |
| argument of perigee: | 85.2378° |
| revolutions per day: | 15.30189630 |
| mean anomaly at epoch: | 274.8759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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