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 63461U 26145.59094684 +.00000000 +00000-0 +38607-3 0 00003
2 63461 43.0016 185.8367 0002205 283.7236 76.3371 15.27580004 03
| Epoch (UTC): | 25 May 2026 14:10:57 |
| Eccentricity: | 0.0002205 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 185.8367° |
| argument of perigee: | 283.7236° |
| revolutions per day: | 15.27580004 |
| mean anomaly at epoch: | 76.3371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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