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 26073.72939228 +.00000000 +00000-0 +17702-3 0 00001
2 25407 71.0120 170.9764 0007062 0.3412 359.7715 14.16192942 06
| Epoch (UTC): | 14 March 2026 17:30:19 |
| Eccentricity: | 0.0007062 |
| inclination: | 71.0120° |
| perigee height: | 833 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 170.9764° |
| argument of perigee: | 0.3412° |
| revolutions per day: | 14.16192942 |
| mean anomaly at epoch: | 359.7715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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