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 26088.20912243 +.00000000 +00000-0 -94285-4 0 00001
2 25407 71.0100 140.5278 0007995 338.0712 22.0068 14.16193902 04
| Epoch (UTC): | 29 March 2026 05:01:08 |
| Eccentricity: | 0.0007995 |
| inclination: | 71.0100° |
| perigee height: | 832 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 140.5278° |
| argument of perigee: | 338.0712° |
| revolutions per day: | 14.16193902 |
| mean anomaly at epoch: | 22.0068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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