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 43880U 26153.84312433 +.00000000 +00000-0 +71901-3 0 00002
2 43880 97.5861 81.5836 0008341 34.8813 325.2980 15.45177103 08
| Epoch (UTC): | 02 June 2026 20:14:05 |
| Eccentricity: | 0.0008341 |
| inclination: | 97.5861° |
| perigee height: | 425 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 81.5836° |
| argument of perigee: | 34.8813° |
| revolutions per day: | 15.45177103 |
| mean anomaly at epoch: | 325.2980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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