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 45201U 26145.40771759 +.00000000 +00000-0 +12742-2 0 00001
2 45201 53.1585 26.8919 0002390 140.5376 219.5800 15.33606930 07
| Epoch (UTC): | 25 May 2026 09:47:06 |
| Eccentricity: | 0.0002390 |
| inclination: | 53.1585° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 26.8919° |
| argument of perigee: | 140.5376° |
| revolutions per day: | 15.33606930 |
| mean anomaly at epoch: | 219.5800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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