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 48685U 26145.19687182 +.00000000 +00000-0 +68513-4 0 00001
2 48685 53.1615 69.0761 0001246 87.8553 272.2591 15.31713817 07
| Epoch (UTC): | 25 May 2026 04:43:29 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 69.0761° |
| argument of perigee: | 87.8553° |
| revolutions per day: | 15.31713817 |
| mean anomaly at epoch: | 272.2591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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