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 61524U 26145.39810523 +.00000000 +00000-0 +26318-4 0 00004
2 61524 53.1601 145.6557 0001271 79.9361 280.1784 15.31700268 08
| Epoch (UTC): | 25 May 2026 09:33:16 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 145.6557° |
| argument of perigee: | 79.9361° |
| revolutions per day: | 15.31700268 |
| mean anomaly at epoch: | 280.1784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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