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 09023U 26087.86446654 +.00000000 +00000-0 +75556-4 0 00005
2 09023 74.0406 294.3815 0016545 24.8746 335.3204 14.41195297 04
| Epoch (UTC): | 28 March 2026 20:44:49 |
| Eccentricity: | 0.0016545 |
| inclination: | 74.0406° |
| perigee height: | 743 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 294.3815° |
| argument of perigee: | 24.8746° |
| revolutions per day: | 14.41195297 |
| mean anomaly at epoch: | 335.3204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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