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 26064.62955866 +.00000000 +00000-0 +65429-3 0 00005
2 00107 28.7780 193.3753 0494866 241.3222 113.6740 14.21703908 03
| Epoch (UTC): | 05 March 2026 15:06:33 |
| Eccentricity: | 0.0494866 |
| inclination: | 28.7780° |
| perigee height: | 463 km |
| apogee height: | 1176 km |
| right ascension of ascending node: | 193.3753° |
| argument of perigee: | 241.3222° |
| revolutions per day: | 14.21703908 |
| mean anomaly at epoch: | 113.6740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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