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 47355U 26145.36071620 +.00000000 +00000-0 +85940-4 0 00000
2 47355 53.1624 14.3892 0001490 90.3984 269.7188 15.31702398 01
| Epoch (UTC): | 25 May 2026 08:39:25 |
| Eccentricity: | 0.0001490 |
| inclination: | 53.1624° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 14.3892° |
| argument of perigee: | 90.3984° |
| revolutions per day: | 15.31702398 |
| mean anomaly at epoch: | 269.7188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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