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 61519U 26145.25819756 +.00000000 +00000-0 -21424-4 0 00004
2 61519 53.1600 144.0738 0001240 83.6299 276.4848 15.42149367 01
| Epoch (UTC): | 25 May 2026 06:11:48 |
| Eccentricity: | 0.0001240 |
| inclination: | 53.1600° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 144.0738° |
| argument of perigee: | 83.6299° |
| revolutions per day: | 15.42149367 |
| mean anomaly at epoch: | 276.4848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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