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 55655U 26144.94191772 +.00000000 +00000-0 +51619-4 0 00002
2 55655 69.9994 332.3067 0002943 268.1427 91.9395 14.98329640 08
| Epoch (UTC): | 24 May 2026 22:36:21 |
| Eccentricity: | 0.0002943 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 332.3067° |
| argument of perigee: | 268.1427° |
| revolutions per day: | 14.98329640 |
| mean anomaly at epoch: | 91.9395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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