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 47379U 26145.05877872 +.00000000 +00000-0 +13387-3 0 00000
2 47379 53.1608 18.3499 0001593 93.3438 266.7746 15.31714701 05
| Epoch (UTC): | 25 May 2026 01:24:38 |
| Eccentricity: | 0.0001593 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 18.3499° |
| argument of perigee: | 93.3438° |
| revolutions per day: | 15.31714701 |
| mean anomaly at epoch: | 266.7746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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