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 47381U 26144.99941480 +.00000000 +00000-0 +39949-3 0 00004
2 47381 53.1599 42.5035 0001244 80.8402 279.2740 15.31700596 07
| Epoch (UTC): | 24 May 2026 23:59:09 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 42.5035° |
| argument of perigee: | 80.8402° |
| revolutions per day: | 15.31700596 |
| mean anomaly at epoch: | 279.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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