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 44949U 26144.90973051 +.00000000 +00000-0 +11118-2 0 00008
2 44949 53.1570 321.0427 0002431 271.5341 88.5391 15.52028491 06
| Epoch (UTC): | 24 May 2026 21:50:00 |
| Eccentricity: | 0.0002431 |
| inclination: | 53.1570° |
| perigee height: | 409 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 321.0427° |
| argument of perigee: | 271.5341° |
| revolutions per day: | 15.52028491 |
| mean anomaly at epoch: | 88.5391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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