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 45183U 26145.12503264 +.00000000 +00000-0 +11312-2 0 00005
2 45183 53.1567 43.6911 0002762 118.1851 241.9430 15.33422970 05
| Epoch (UTC): | 25 May 2026 03:00:02 |
| Eccentricity: | 0.0002762 |
| inclination: | 53.1567° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 43.6911° |
| argument of perigee: | 118.1851° |
| revolutions per day: | 15.33422970 |
| mean anomaly at epoch: | 241.9430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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