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 43800U 26145.59132457 +.00000000 +00000-0 +40507-3 0 00001
2 43800 97.4374 199.8356 0010921 31.4752 328.7133 15.17401707 07
| Epoch (UTC): | 25 May 2026 14:11:30 |
| Eccentricity: | 0.0010921 |
| inclination: | 97.4374° |
| perigee height: | 506 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 199.8356° |
| argument of perigee: | 31.4752° |
| revolutions per day: | 15.17401707 |
| mean anomaly at epoch: | 328.7133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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