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 37363U 26162.19924053 +.00000000 +00000-0 +32870-3 0 00008
2 37363 99.3545 301.5887 0107197 205.3745 154.2223 15.65234952 03
| Epoch (UTC): | 11 June 2026 04:46:54 |
| Eccentricity: | 0.0107197 |
| inclination: | 99.3545° |
| perigee height: | 300 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 301.5887° |
| argument of perigee: | 205.3745° |
| revolutions per day: | 15.65234952 |
| mean anomaly at epoch: | 154.2223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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