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 47378U 26145.37579841 +.00000000 +00000-0 +44469-4 0 00005
2 47378 53.1601 17.4955 0001320 101.9654 258.1496 15.31704414 05
| Epoch (UTC): | 25 May 2026 09:01:08 |
| Eccentricity: | 0.0001320 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 17.4955° |
| argument of perigee: | 101.9654° |
| revolutions per day: | 15.31704414 |
| mean anomaly at epoch: | 258.1496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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