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 25019U 26106.81620148 +.00000000 +00000-0 +00000-0 0 00005
2 25019 12.7126 22.1767 0005841 321.2135 42.9791 1.00273862 09
| Epoch (UTC): | 16 April 2026 19:35:19 |
| Eccentricity: | 0.0005841 |
| inclination: | 12.7126° |
| perigee height: | 35761 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 22.1767° |
| argument of perigee: | 321.2135° |
| revolutions per day: | 1.00273862 |
| mean anomaly at epoch: | 42.9791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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