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 55459U 26145.01045265 +.00000000 +00000-0 -29110-4 0 00000
2 55459 43.0038 257.7604 0001100 271.1126 88.9599 15.27584446 05
| Epoch (UTC): | 25 May 2026 00:15:03 |
| Eccentricity: | 0.0001100 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 257.7604° |
| argument of perigee: | 271.1126° |
| revolutions per day: | 15.27584446 |
| mean anomaly at epoch: | 88.9599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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