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 23657U 26142.27212083 +.00000000 +00000-0 +10802-3 0 00000
2 23657 82.5243 66.6986 0020030 53.5765 306.7300 14.94592684 07
| Epoch (UTC): | 22 May 2026 06:31:51 |
| Eccentricity: | 0.0020030 |
| inclination: | 82.5243° |
| perigee height: | 570 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 66.6986° |
| argument of perigee: | 53.5765° |
| revolutions per day: | 14.94592684 |
| mean anomaly at epoch: | 306.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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