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 55948U 26145.21845758 +.00000000 +00000-0 +74188-4 0 00004
2 55948 70.0001 71.6144 0002883 269.1535 90.9294 14.98331574 04
| Epoch (UTC): | 25 May 2026 05:14:34 |
| Eccentricity: | 0.0002883 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.6144° |
| argument of perigee: | 269.1535° |
| revolutions per day: | 14.98331574 |
| mean anomaly at epoch: | 90.9294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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