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 26158.76016186 +.00000000 +00000-0 +75749-4 0 00002
2 10096 75.8332 289.5068 0040134 126.5322 233.9577 14.92124917 03
| Epoch (UTC): | 07 June 2026 18:14:37 |
| Eccentricity: | 0.0040134 |
| inclination: | 75.8332° |
| perigee height: | 563 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 289.5068° |
| argument of perigee: | 126.5322° |
| revolutions per day: | 14.92124917 |
| mean anomaly at epoch: | 233.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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