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 26158.84179500 +.00000000 +00000-0 +51466-4 0 00003
2 25407 71.0121 351.9840 0009535 252.9402 107.0677 14.16204661 07
| Epoch (UTC): | 07 June 2026 20:12:11 |
| Eccentricity: | 0.0009535 |
| inclination: | 71.0121° |
| perigee height: | 831 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 351.9840° |
| argument of perigee: | 252.9402° |
| revolutions per day: | 14.16204661 |
| mean anomaly at epoch: | 107.0677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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