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 05730U 26040.95651395 +.00000000 +00000-0 +68863-3 0 00007
2 05730 73.8854 227.5247 0553659 199.8509 158.0330 14.36997872 01
| Epoch (UTC): | 09 February 2026 22:57:22 |
| Eccentricity: | 0.0553659 |
| inclination: | 73.8854° |
| perigee height: | 373 km |
| apogee height: | 1164 km |
| right ascension of ascending node: | 227.5247° |
| argument of perigee: | 199.8509° |
| revolutions per day: | 14.36997872 |
| mean anomaly at epoch: | 158.0330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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