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 19120U 26021.48836078 +.00000000 +00000-0 +65015-4 0 00002
2 19120 71.0140 168.3537 0020053 48.4017 311.8822 14.19608321 05
| Epoch (UTC): | 21 January 2026 11:43:14 |
| Eccentricity: | 0.0020053 |
| inclination: | 71.0140° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 168.3537° |
| argument of perigee: | 48.4017° |
| revolutions per day: | 14.19608321 |
| mean anomaly at epoch: | 311.8822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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