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 26156.86408821 +.00000000 +00000-0 +10644-3 0 00006
2 25407 71.0121 356.1436 0009546 255.0716 104.9350 14.16204086 04
| Epoch (UTC): | 05 June 2026 20:44:17 |
| Eccentricity: | 0.0009546 |
| inclination: | 71.0121° |
| perigee height: | 831 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 356.1436° |
| argument of perigee: | 255.0716° |
| revolutions per day: | 14.16204086 |
| mean anomaly at epoch: | 104.9350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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