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 26145.37354978 +.00000000 +00000-0 +95990-3 0 00003
2 43879 97.5895 78.9131 0006243 58.5037 301.6829 15.61030495 01
| Epoch (UTC): | 25 May 2026 08:57:54 |
| Eccentricity: | 0.0006243 |
| inclination: | 97.5895° |
| perigee height: | 380 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 78.9131° |
| argument of perigee: | 58.5037° |
| revolutions per day: | 15.61030495 |
| mean anomaly at epoch: | 301.6829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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