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 45379U 26145.37604234 +.00000000 +00000-0 +52094-3 0 00001
2 45379 53.0385 110.4836 0004870 48.7374 311.4064 15.74807880 06
| Epoch (UTC): | 25 May 2026 09:01:30 |
| Eccentricity: | 0.0004870 |
| inclination: | 53.0385° |
| perigee height: | 342 km |
| apogee height: | 348 km |
| right ascension of ascending node: | 110.4836° |
| argument of perigee: | 48.7374° |
| revolutions per day: | 15.74807880 |
| mean anomaly at epoch: | 311.4064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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