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 44350U 26145.39818704 +.00000000 +00000-0 +17254-3 0 00009
2 44350 23.9978 248.1263 0000746 291.5263 68.5158 14.96391735 08
| Epoch (UTC): | 25 May 2026 09:33:23 |
| Eccentricity: | 0.0000746 |
| inclination: | 23.9978° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 248.1263° |
| argument of perigee: | 291.5263° |
| revolutions per day: | 14.96391735 |
| mean anomaly at epoch: | 68.5158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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