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 26145.33188987 +.00000000 +00000-0 +00000-0 0 00005
2 25019 12.7586 21.8980 0004750 336.1676 252.1840 1.00272616 01
| Epoch (UTC): | 25 May 2026 07:57:55 |
| Eccentricity: | 0.0004750 |
| inclination: | 12.7586° |
| perigee height: | 35766 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 21.8980° |
| argument of perigee: | 336.1676° |
| revolutions per day: | 1.00272616 |
| mean anomaly at epoch: | 252.1840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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