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 43773U 26145.56380538 +.00000000 +00000-0 +21788-3 0 00002
2 43773 97.3984 188.8068 0011952 70.3895 289.8625 15.13156258 02
| Epoch (UTC): | 25 May 2026 13:31:52 |
| Eccentricity: | 0.0011952 |
| inclination: | 97.3984° |
| perigee height: | 518 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 188.8068° |
| argument of perigee: | 70.3895° |
| revolutions per day: | 15.13156258 |
| mean anomaly at epoch: | 289.8625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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