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 26041.93119128 +.00000000 +00000-0 +68598-3 0 00004
2 05730 73.8852 225.7048 0553536 197.8335 160.2700 14.37023859 09
| Epoch (UTC): | 10 February 2026 22:20:54 |
| Eccentricity: | 0.0553536 |
| inclination: | 73.8852° |
| perigee height: | 373 km |
| apogee height: | 1164 km |
| right ascension of ascending node: | 225.7048° |
| argument of perigee: | 197.8335° |
| revolutions per day: | 14.37023859 |
| mean anomaly at epoch: | 160.2700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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