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 26112.24072969 +.00000000 +00000-0 +13956-3 0 00006
2 44881 97.7547 185.8342 0011973 271.8107 88.1738 14.86429024 09
| Epoch (UTC): | 22 April 2026 05:46:39 |
| Eccentricity: | 0.0011973 |
| inclination: | 97.7547° |
| perigee height: | 601 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 185.8342° |
| argument of perigee: | 271.8107° |
| revolutions per day: | 14.86429024 |
| mean anomaly at epoch: | 88.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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