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 47400U 26145.06343911 +.00000000 +00000-0 +32311-4 0 00007
2 47400 53.1610 18.3127 0001135 84.4387 275.6744 15.31699694 07
| Epoch (UTC): | 25 May 2026 01:31:21 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 18.3127° |
| argument of perigee: | 84.4387° |
| revolutions per day: | 15.31699694 |
| mean anomaly at epoch: | 275.6744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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