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 44725U 26145.33850095 +.00000000 +00000-0 +96782-3 0 00001
2 44725 53.1584 202.7349 0003992 17.7100 342.4049 15.52332672 08
| Epoch (UTC): | 25 May 2026 08:07:26 |
| Eccentricity: | 0.0003992 |
| inclination: | 53.1584° |
| perigee height: | 407 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 202.7349° |
| argument of perigee: | 17.7100° |
| revolutions per day: | 15.52332672 |
| mean anomaly at epoch: | 342.4049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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