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 61513U 26145.32313044 +.00000000 +00000-0 +13571-4 0 00008
2 61513 53.1602 146.6208 0001173 88.0666 272.0469 15.30191849 09
| Epoch (UTC): | 25 May 2026 07:45:18 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.6208° |
| argument of perigee: | 88.0666° |
| revolutions per day: | 15.30191849 |
| mean anomaly at epoch: | 272.0469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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