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 00107U 26017.58184875 +.00000000 +00000-0 +32460-3 0 00001
2 00107 28.7787 104.3603 0497241 162.2871 199.5723 14.21188347 05
| Epoch (UTC): | 17 January 2026 13:57:51 |
| Eccentricity: | 0.0497241 |
| inclination: | 28.7787° |
| perigee height: | 463 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 104.3603° |
| argument of perigee: | 162.2871° |
| revolutions per day: | 14.21188347 |
| mean anomaly at epoch: | 199.5723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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