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 44231U 26145.61230616 +.00000000 +00000-0 +00000-0 0 00000
2 44231 1.6034 74.4729 0010590 281.7458 251.8998 1.00269140 08
| Epoch (UTC): | 25 May 2026 14:41:43 |
| Eccentricity: | 0.0010590 |
| inclination: | 1.6034° |
| perigee height: | 35743 km |
| apogee height: | 35832 km |
| right ascension of ascending node: | 74.4729° |
| argument of perigee: | 281.7458° |
| revolutions per day: | 1.00269140 |
| mean anomaly at epoch: | 251.8998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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