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 55425U 26145.54599441 +.00000000 +00000-0 +28915-4 0 00002
2 55425 69.9992 250.7060 0003271 271.6352 88.4432 14.98331369 02
| Epoch (UTC): | 25 May 2026 13:06:13 |
| Eccentricity: | 0.0003271 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.7060° |
| argument of perigee: | 271.6352° |
| revolutions per day: | 14.98331369 |
| mean anomaly at epoch: | 88.4432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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