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 55573U 26145.12467198 +.00000000 +00000-0 +76330-4 0 00007
2 55573 43.0002 296.8544 0001208 272.0835 87.9878 15.27569831 06
| Epoch (UTC): | 25 May 2026 02:59:31 |
| Eccentricity: | 0.0001208 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 296.8544° |
| argument of perigee: | 272.0835° |
| revolutions per day: | 15.27569831 |
| mean anomaly at epoch: | 87.9878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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