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 47371U 26145.21570911 +.00000000 +00000-0 +65661-4 0 00007
2 47371 53.1627 70.4290 0001266 92.3480 267.7666 15.31719453 00
| Epoch (UTC): | 25 May 2026 05:10:37 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.1627° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 70.4290° |
| argument of perigee: | 92.3480° |
| revolutions per day: | 15.31719453 |
| mean anomaly at epoch: | 267.7666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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