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 47179U 26145.49616743 +.00000000 +00000-0 +13077-2 0 00009
2 47179 53.1592 309.7182 0000973 330.4607 29.6340 15.32869022 09
| Epoch (UTC): | 25 May 2026 11:54:28 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1592° |
| perigee height: | 467 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 309.7182° |
| argument of perigee: | 330.4607° |
| revolutions per day: | 15.32869022 |
| mean anomaly at epoch: | 29.6340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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