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 47202U 26145.60175441 +.00000000 +00000-0 +00000-0 0 00004
2 47202 0.0138 301.8326 0002530 115.9334 132.8504 1.00272493 09
| Epoch (UTC): | 25 May 2026 14:26:31 |
| Eccentricity: | 0.0002530 |
| inclination: | 0.0138° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 301.8326° |
| argument of perigee: | 115.9334° |
| revolutions per day: | 1.00272493 |
| mean anomaly at epoch: | 132.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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