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 47672U 26145.66668980 +.00000000 +00000-0 +82685-3 0 00008
2 47672 53.1436 343.5074 0007255 254.0274 84.0638 15.95589628 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0007255 |
| inclination: | 53.1436° |
| perigee height: | 282 km |
| apogee height: | 292 km |
| right ascension of ascending node: | 343.5074° |
| argument of perigee: | 254.0274° |
| revolutions per day: | 15.95589628 |
| mean anomaly at epoch: | 84.0638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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