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 41250U 26029.38601981 +.00000000 +00000-0 +23296-1 0 00003
2 41250 98.9803 242.2291 0003706 12.7337 347.3991 15.28672424 09
| Epoch (UTC): | 29 January 2026 09:15:52 |
| Eccentricity: | 0.0003706 |
| inclination: | 98.9803° |
| perigee height: | 477 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 242.2291° |
| argument of perigee: | 12.7337° |
| revolutions per day: | 15.28672424 |
| mean anomaly at epoch: | 347.3991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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