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 45532U 26145.19698793 +.00000000 +00000-0 +49065-3 0 00009
2 45532 53.0448 71.3090 0004509 64.5789 295.5692 15.66284671 06
| Epoch (UTC): | 25 May 2026 04:43:39 |
| Eccentricity: | 0.0004509 |
| inclination: | 53.0448° |
| perigee height: | 367 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 71.3090° |
| argument of perigee: | 64.5789° |
| revolutions per day: | 15.66284671 |
| mean anomaly at epoch: | 295.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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