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 26074.05088078 +.00000000 +00000-0 +85242-4 0 00007
2 09023 74.0436 319.9465 0016073 54.9922 305.2740 14.41188210 06
| Epoch (UTC): | 15 March 2026 01:13:16 |
| Eccentricity: | 0.0016073 |
| inclination: | 74.0436° |
| perigee height: | 743 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 319.9465° |
| argument of perigee: | 54.9922° |
| revolutions per day: | 14.41188210 |
| mean anomaly at epoch: | 305.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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