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 26040.95562903 +.00000000 +00000-0 +61559-4 0 00002
2 25407 71.0082 239.8975 0005424 59.6725 300.4934 14.16185342 08
| Epoch (UTC): | 09 February 2026 22:56:06 |
| Eccentricity: | 0.0005424 |
| inclination: | 71.0082° |
| perigee height: | 834 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 239.8975° |
| argument of perigee: | 59.6725° |
| revolutions per day: | 14.16185342 |
| mean anomaly at epoch: | 300.4934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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