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 26041.94449610 +.00000000 +00000-0 +99116-4 0 00001
2 25407 71.0082 237.8177 0005470 57.6741 302.4911 14.16185665 02
| Epoch (UTC): | 10 February 2026 22:40:04 |
| Eccentricity: | 0.0005470 |
| inclination: | 71.0082° |
| perigee height: | 834 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 237.8177° |
| argument of perigee: | 57.6741° |
| revolutions per day: | 14.16185665 |
| mean anomaly at epoch: | 302.4911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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