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 44351U 26144.75373333 +.00000000 +00000-0 +16496-3 0 00000
2 44351 23.9993 306.7842 0000323 293.4166 66.6301 14.96386186 07
| Epoch (UTC): | 24 May 2026 18:05:22 |
| Eccentricity: | 0.0000323 |
| inclination: | 23.9993° |
| perigee height: | 578 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 306.7842° |
| argument of perigee: | 293.4166° |
| revolutions per day: | 14.96386186 |
| mean anomaly at epoch: | 66.6301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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