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 45701U 26145.40019250 +.00000000 +00000-0 +12393-2 0 00009
2 45701 53.1551 40.0765 0002923 120.4173 239.7118 15.32649518 00
| Epoch (UTC): | 25 May 2026 09:36:16 |
| Eccentricity: | 0.0002923 |
| inclination: | 53.1551° |
| perigee height: | 466 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 40.0765° |
| argument of perigee: | 120.4173° |
| revolutions per day: | 15.32649518 |
| mean anomaly at epoch: | 239.7118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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