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 43881U 26145.33027596 +.00000000 +00000-0 +10487-2 0 00002
2 43881 97.6122 84.1167 0006682 91.6626 268.5400 15.67919519 00
| Epoch (UTC): | 25 May 2026 07:55:35 |
| Eccentricity: | 0.0006682 |
| inclination: | 97.6122° |
| perigee height: | 360 km |
| apogee height: | 369 km |
| right ascension of ascending node: | 84.1167° |
| argument of perigee: | 91.6626° |
| revolutions per day: | 15.67919519 |
| mean anomaly at epoch: | 268.5400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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