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 55403U 26145.51654800 +.00000000 +00000-0 +68286-4 0 00001
2 55403 69.9992 230.7326 0003381 268.9646 91.1126 14.98333411 09
| Epoch (UTC): | 25 May 2026 12:23:49 |
| Eccentricity: | 0.0003381 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.7326° |
| argument of perigee: | 268.9646° |
| revolutions per day: | 14.98333411 |
| mean anomaly at epoch: | 91.1126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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