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 44115U 26145.07820028 +.00000000 +00000-0 +00000-0 0 00003
2 44115 0.0530 0.0660 0002765 63.9912 295.9707 5.00115354 00
| Epoch (UTC): | 25 May 2026 01:52:36 |
| Eccentricity: | 0.0002765 |
| inclination: | 0.0530° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 0.0660° |
| argument of perigee: | 63.9912° |
| revolutions per day: | 5.00115354 |
| mean anomaly at epoch: | 295.9707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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