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 47377U 26145.48170125 +.00000000 +00000-0 +17765-3 0 00006
2 47377 53.1588 69.1206 0000984 62.9351 297.1751 15.31714437 09
| Epoch (UTC): | 25 May 2026 11:33:38 |
| Eccentricity: | 0.0000984 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 69.1206° |
| argument of perigee: | 62.9351° |
| revolutions per day: | 15.31714437 |
| mean anomaly at epoch: | 297.1751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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