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 19420U 26106.24184294 +.00000000 +00000-0 +72064-4 0 00001
2 19420 90.0471 21.0739 0092390 245.0553 236.7765 13.42603615 05
| Epoch (UTC): | 16 April 2026 05:48:15 |
| Eccentricity: | 0.0092390 |
| inclination: | 90.0471° |
| perigee height: | 1031 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.0739° |
| argument of perigee: | 245.0553° |
| revolutions per day: | 13.42603615 |
| mean anomaly at epoch: | 236.7765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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