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 43188U 26145.30164323 +.00000000 +00000-0 +23888-3 0 00009
2 43188 97.5396 50.4271 0010629 93.2485 266.9964 15.16424413 06
| Epoch (UTC): | 25 May 2026 07:14:21 |
| Eccentricity: | 0.0010629 |
| inclination: | 97.5396° |
| perigee height: | 509 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 50.4271° |
| argument of perigee: | 93.2485° |
| revolutions per day: | 15.16424413 |
| mean anomaly at epoch: | 266.9964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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