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 19119U 26072.43210595 +.00000000 +00000-0 +17958-3 0 00003
2 19119 71.0012 238.0550 0013405 245.9200 134.9564 14.15740598 08
| Epoch (UTC): | 13 March 2026 10:22:13 |
| Eccentricity: | 0.0013405 |
| inclination: | 71.0012° |
| perigee height: | 830 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 238.0550° |
| argument of perigee: | 245.9200° |
| revolutions per day: | 14.15740598 |
| mean anomaly at epoch: | 134.9564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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