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 49459U 26145.22749572 +.00000000 +00000-0 -43958-4 0 00004
2 49459 53.2126 235.5291 0000965 124.4486 235.6597 15.08827934 02
| Epoch (UTC): | 25 May 2026 05:27:35 |
| Eccentricity: | 0.0000965 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 235.5291° |
| argument of perigee: | 124.4486° |
| revolutions per day: | 15.08827934 |
| mean anomaly at epoch: | 235.6597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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