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 26162.59335294 +.00000000 +00000-0 +17905-3 0 00006
2 23088 70.9993 233.6789 0003135 191.8567 168.2483 14.15021446 07
| Epoch (UTC): | 11 June 2026 14:14:25 |
| Eccentricity: | 0.0003135 |
| inclination: | 70.9993° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 233.6789° |
| argument of perigee: | 191.8567° |
| revolutions per day: | 14.15021446 |
| mean anomaly at epoch: | 168.2483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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