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 23088U 26021.49261894 +.00000000 +00000-0 +22032-4 0 00001
2 23088 70.9998 170.0038 0003868 330.1775 29.9127 14.15007019 03
| Epoch (UTC): | 21 January 2026 11:49:22 |
| Eccentricity: | 0.0003868 |
| inclination: | 70.9998° |
| perigee height: | 839 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 170.0038° |
| argument of perigee: | 330.1775° |
| revolutions per day: | 14.15007019 |
| mean anomaly at epoch: | 29.9127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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