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 44881U 26075.28306023 +.00000000 +00000-0 +13017-3 0 00007
2 44881 97.7602 149.7644 0014449 37.6888 322.5338 14.86356230 09
| Epoch (UTC): | 16 March 2026 06:47:36 |
| Eccentricity: | 0.0014449 |
| inclination: | 97.7602° |
| perigee height: | 599 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 149.7644° |
| argument of perigee: | 37.6888° |
| revolutions per day: | 14.86356230 |
| mean anomaly at epoch: | 322.5338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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