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 55434U 26145.36680383 +.00000000 +00000-0 +62200-4 0 00003
2 55434 69.9989 271.1424 0003157 269.3833 90.6964 14.98334150 06
| Epoch (UTC): | 25 May 2026 08:48:11 |
| Eccentricity: | 0.0003157 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.1424° |
| argument of perigee: | 269.3833° |
| revolutions per day: | 14.98334150 |
| mean anomaly at epoch: | 90.6964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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