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 26110.14437255 +.00000000 +00000-0 -18908-4 0 00000
2 23190 74.0272 150.9991 0018404 134.9232 225.3384 13.74385618 07
| Epoch (UTC): | 20 April 2026 03:27:53 |
| Eccentricity: | 0.0018404 |
| inclination: | 74.0272° |
| perigee height: | 970 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 150.9991° |
| argument of perigee: | 134.9232° |
| revolutions per day: | 13.74385618 |
| mean anomaly at epoch: | 225.3384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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