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 26160.29563252 +.00000000 +00000-0 +89376-3 0 00009
2 43879 97.5882 94.9178 0001911 49.1516 310.9907 15.63889972 05
| Epoch (UTC): | 09 June 2026 07:05:42 |
| Eccentricity: | 0.0001911 |
| inclination: | 97.5882° |
| perigee height: | 375 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 94.9178° |
| argument of perigee: | 49.1516° |
| revolutions per day: | 15.63889972 |
| mean anomaly at epoch: | 310.9907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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