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 48688U 26145.50452486 +.00000000 +00000-0 +10711-3 0 00002
2 48688 53.1591 67.9131 0001178 83.6931 276.4205 15.31703179 07
| Epoch (UTC): | 25 May 2026 12:06:30 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 67.9131° |
| argument of perigee: | 83.6931° |
| revolutions per day: | 15.31703179 |
| mean anomaly at epoch: | 276.4205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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