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 26065.23513245 +.00000000 +00000-0 +12911-3 0 00008
2 09023 74.0446 336.2590 0015863 74.6331 285.6576 14.41182529 02
| Epoch (UTC): | 06 March 2026 05:38:35 |
| Eccentricity: | 0.0015863 |
| inclination: | 74.0446° |
| perigee height: | 743 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 336.2590° |
| argument of perigee: | 74.6331° |
| revolutions per day: | 14.41182529 |
| mean anomaly at epoch: | 285.6576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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