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 26103.40044632 +.00000000 +00000-0 +00000-0 0 00005
2 25019 12.7082 22.2006 0005858 323.2524 247.8587 1.00273344 03
| Epoch (UTC): | 13 April 2026 09:36:38 |
| Eccentricity: | 0.0005858 |
| inclination: | 12.7082° |
| perigee height: | 35761 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 22.2006° |
| argument of perigee: | 323.2524° |
| revolutions per day: | 1.00273344 |
| mean anomaly at epoch: | 247.8587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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