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 45555U 26145.12470186 +.00000000 +00000-0 +44541-3 0 00005
2 45555 53.0420 54.0079 0005223 46.0102 314.1342 15.65656562 05
| Epoch (UTC): | 25 May 2026 02:59:34 |
| Eccentricity: | 0.0005223 |
| inclination: | 53.0420° |
| perigee height: | 368 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 54.0079° |
| argument of perigee: | 46.0102° |
| revolutions per day: | 15.65656562 |
| mean anomaly at epoch: | 314.1342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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