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 26021.46083777 +.00000000 +00000-0 +20573-3 0 00004
2 25407 71.0113 280.8958 0005218 101.3236 258.8474 14.16184331 05
| Epoch (UTC): | 21 January 2026 11:03:36 |
| Eccentricity: | 0.0005218 |
| inclination: | 71.0113° |
| perigee height: | 835 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 280.8958° |
| argument of perigee: | 101.3236° |
| revolutions per day: | 14.16184331 |
| mean anomaly at epoch: | 258.8474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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