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 01328U 26088.13975028 +.00000000 +00000-0 +13647-3 0 00000
2 01328 41.1866 359.7855 0242689 249.7486 107.7024 13.38922484 00
| Epoch (UTC): | 29 March 2026 03:21:14 |
| Eccentricity: | 0.0242689 |
| inclination: | 41.1866° |
| perigee height: | 931 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 359.7855° |
| argument of perigee: | 249.7486° |
| revolutions per day: | 13.38922484 |
| mean anomaly at epoch: | 107.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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