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 19325U 26071.73618766 +.00000000 +00000-0 +73668-4 0 00007
2 19325 82.9548 171.2076 0032307 294.2472 230.2371 13.77909593 08
| Epoch (UTC): | 12 March 2026 17:40:06 |
| Eccentricity: | 0.0032307 |
| inclination: | 82.9548° |
| perigee height: | 948 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 171.2076° |
| argument of perigee: | 294.2472° |
| revolutions per day: | 13.77909593 |
| mean anomaly at epoch: | 230.2371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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