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 61509U 26145.37524022 +.00000000 +00000-0 +10586-4 0 00001
2 61509 53.1595 133.4443 0001300 79.9678 280.1469 15.30188252 08
| Epoch (UTC): | 25 May 2026 09:00:20 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.4443° |
| argument of perigee: | 79.9678° |
| revolutions per day: | 15.30188252 |
| mean anomaly at epoch: | 280.1469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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