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 26106.94096838 +.00000000 +00000-0 +58692-4 0 00003
2 01328 41.1840 279.3424 0241863 347.2416 12.2293 13.38923509 08
| Epoch (UTC): | 16 April 2026 22:34:59 |
| Eccentricity: | 0.0241863 |
| inclination: | 41.1840° |
| perigee height: | 932 km |
| apogee height: | 1294 km |
| right ascension of ascending node: | 279.3424° |
| argument of perigee: | 347.2416° |
| revolutions per day: | 13.38923509 |
| mean anomaly at epoch: | 12.2293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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