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 57944U 26144.90517666 +.00000000 +00000-0 +37380-4 0 00004
2 57944 53.1615 30.1006 0000847 88.9651 271.1448 15.33551625 01
| Epoch (UTC): | 24 May 2026 21:43:27 |
| Eccentricity: | 0.0000847 |
| inclination: | 53.1615° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 30.1006° |
| argument of perigee: | 88.9651° |
| revolutions per day: | 15.33551625 |
| mean anomaly at epoch: | 271.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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