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 26100.14608281 +.00000000 +00000-0 +16441-3 0 00009
2 25407 71.0087 115.4229 0008546 323.0716 36.9818 14.16196360 04
| Epoch (UTC): | 10 April 2026 03:30:21 |
| Eccentricity: | 0.0008546 |
| inclination: | 71.0087° |
| perigee height: | 832 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 115.4229° |
| argument of perigee: | 323.0716° |
| revolutions per day: | 14.16196360 |
| mean anomaly at epoch: | 36.9818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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