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 55436U 26145.37098583 +.00000000 +00000-0 +30815-4 0 00008
2 55436 69.9991 271.1571 0003075 269.8124 90.2683 14.98339496 03
| Epoch (UTC): | 25 May 2026 08:54:13 |
| Eccentricity: | 0.0003075 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.1571° |
| argument of perigee: | 269.8124° |
| revolutions per day: | 14.98339496 |
| mean anomaly at epoch: | 90.2683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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