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 44035U 26145.52198508 +.00000000 +00000-0 +00000-0 0 00005
2 44035 0.0511 104.8986 0001688 250.6236 123.4107 1.00272803 09
| Epoch (UTC): | 25 May 2026 12:31:39 |
| Eccentricity: | 0.0001688 |
| inclination: | 0.0511° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 104.8986° |
| argument of perigee: | 250.6236° |
| revolutions per day: | 1.00272803 |
| mean anomaly at epoch: | 123.4107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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