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 47971U 26145.05871060 +.00000000 +00000-0 +38816-3 0 00005
2 47971 44.9831 20.4275 0003724 198.4194 161.6561 15.45542168 08
| Epoch (UTC): | 25 May 2026 01:24:32 |
| Eccentricity: | 0.0003724 |
| inclination: | 44.9831° |
| perigee height: | 427 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 20.4275° |
| argument of perigee: | 198.4194° |
| revolutions per day: | 15.45542168 |
| mean anomaly at epoch: | 161.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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