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 26037.61463633 +.00000000 +00000-0 +64549-3 0 00009
2 05730 73.8853 233.7648 0554050 206.7721 150.3835 14.36912669 00
| Epoch (UTC): | 06 February 2026 14:45:04 |
| Eccentricity: | 0.0554050 |
| inclination: | 73.8853° |
| perigee height: | 373 km |
| apogee height: | 1165 km |
| right ascension of ascending node: | 233.7648° |
| argument of perigee: | 206.7721° |
| revolutions per day: | 14.36912669 |
| mean anomaly at epoch: | 150.3835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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