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 28117U 26145.74124975 +.00000000 +00000-0 +00000-0 0 00009
2 28117 8.9381 33.9428 0002547 42.6171 149.0907 1.00273170 09
| Epoch (UTC): | 25 May 2026 17:47:23 |
| Eccentricity: | 0.0002547 |
| inclination: | 8.9381° |
| perigee height: | 35775 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 33.9428° |
| argument of perigee: | 42.6171° |
| revolutions per day: | 1.00273170 |
| mean anomaly at epoch: | 149.0907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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