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 47799U 26145.55037199 +.00000000 +00000-0 +32898-4 0 00000
2 47799 53.1580 234.6620 0001429 94.5545 265.5619 15.31703689 08
| Epoch (UTC): | 25 May 2026 13:12:32 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 234.6620° |
| argument of perigee: | 94.5545° |
| revolutions per day: | 15.31703689 |
| mean anomaly at epoch: | 265.5619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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