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 26044.90100917 +.00000000 +00000-0 +59901-3 0 00001
2 00107 28.7769 307.0426 0495664 57.1824 307.5499 14.21504319 09
| Epoch (UTC): | 13 February 2026 21:37:27 |
| Eccentricity: | 0.0495664 |
| inclination: | 28.7769° |
| perigee height: | 463 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 307.0426° |
| argument of perigee: | 57.1824° |
| revolutions per day: | 14.21504319 |
| mean anomaly at epoch: | 307.5499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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