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 26038.93748542 +.00000000 +00000-0 +63342-3 0 00000
2 05730 73.8855 231.2952 0553834 204.0340 153.4050 14.36945340 05
| Epoch (UTC): | 07 February 2026 22:29:58 |
| Eccentricity: | 0.0553834 |
| inclination: | 73.8855° |
| perigee height: | 373 km |
| apogee height: | 1164 km |
| right ascension of ascending node: | 231.2952° |
| argument of perigee: | 204.0340° |
| revolutions per day: | 14.36945340 |
| mean anomaly at epoch: | 153.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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