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 44343U 26144.85311209 +.00000000 +00000-0 +23123-3 0 00001
2 44343 24.0004 339.1169 0000942 29.1728 330.8828 15.09596798 07
| Epoch (UTC): | 24 May 2026 20:28:28 |
| Eccentricity: | 0.0000942 |
| inclination: | 24.0004° |
| perigee height: | 537 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 339.1169° |
| argument of perigee: | 29.1728° |
| revolutions per day: | 15.09596798 |
| mean anomaly at epoch: | 330.8828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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