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 25893U 26074.65681432 +.00000000 +00000-0 +53346-4 0 00009
2 25893 82.9303 166.9991 0029306 162.0577 308.3683 13.76827950 02
| Epoch (UTC): | 15 March 2026 15:45:48 |
| Eccentricity: | 0.0029306 |
| inclination: | 82.9303° |
| perigee height: | 954 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 166.9991° |
| argument of perigee: | 162.0577° |
| revolutions per day: | 13.76827950 |
| mean anomaly at epoch: | 308.3683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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