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 25407U 26158.91242733 +.00000000 +00000-0 +50740-4 0 00004
2 25407 71.0121 351.8354 0009531 252.8605 107.1475 14.16204706 03
| Epoch (UTC): | 07 June 2026 21:53:53 |
| Eccentricity: | 0.0009531 |
| inclination: | 71.0121° |
| perigee height: | 831 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 351.8354° |
| argument of perigee: | 252.8605° |
| revolutions per day: | 14.16204706 |
| mean anomaly at epoch: | 107.1475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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