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 55400U 26145.52072263 +.00000000 +00000-0 +45436-4 0 00008
2 55400 69.9992 230.7421 0003511 269.4618 90.6138 14.98333008 01
| Epoch (UTC): | 25 May 2026 12:29:50 |
| Eccentricity: | 0.0003511 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.7421° |
| argument of perigee: | 269.4618° |
| revolutions per day: | 14.98333008 |
| mean anomaly at epoch: | 90.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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