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 43879U 26077.75193913 +.00000000 +00000-0 +77555-3 0 00006
2 43879 97.5914 7.0026 0002060 255.2985 104.8039 15.52234542 05
| Epoch (UTC): | 18 March 2026 18:02:47 |
| Eccentricity: | 0.0002060 |
| inclination: | 97.5914° |
| perigee height: | 409 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 7.0026° |
| argument of perigee: | 255.2985° |
| revolutions per day: | 15.52234542 |
| mean anomaly at epoch: | 104.8039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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