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 25982U 26145.41948819 +.00000000 +00000-0 +23635-3 0 00003
2 25982 45.0158 281.0055 0005718 289.9084 70.1148 14.37096110 06
| Epoch (UTC): | 25 May 2026 10:04:03 |
| Eccentricity: | 0.0005718 |
| inclination: | 45.0158° |
| perigee height: | 764 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 281.0055° |
| argument of perigee: | 289.9084° |
| revolutions per day: | 14.37096110 |
| mean anomaly at epoch: | 70.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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