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 23190U 26159.49425307 +.00000000 +00000-0 +56704-4 0 00001
2 23190 74.0301 69.1769 0018580 38.3813 321.8624 13.74384853 00
| Epoch (UTC): | 08 June 2026 11:51:43 |
| Eccentricity: | 0.0018580 |
| inclination: | 74.0301° |
| perigee height: | 970 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 69.1769° |
| argument of perigee: | 38.3813° |
| revolutions per day: | 13.74384853 |
| mean anomaly at epoch: | 321.8624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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