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 10096U 26075.27941066 +.00000000 +00000-0 +76118-4 0 00001
2 10096 75.8306 78.6196 0041184 338.7828 21.1654 14.92018252 04
| Epoch (UTC): | 16 March 2026 06:42:21 |
| Eccentricity: | 0.0041184 |
| inclination: | 75.8306° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 78.6196° |
| argument of perigee: | 338.7828° |
| revolutions per day: | 14.92018252 |
| mean anomaly at epoch: | 21.1654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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