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 26088.17416024 +.00000000 +00000-0 +18436-3 0 00000
2 23657 82.5212 118.2467 0017374 228.7281 131.2444 14.94435077 09
| Epoch (UTC): | 29 March 2026 04:10:47 |
| Eccentricity: | 0.0017374 |
| inclination: | 82.5212° |
| perigee height: | 572 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 118.2467° |
| argument of perigee: | 228.7281° |
| revolutions per day: | 14.94435077 |
| mean anomaly at epoch: | 131.2444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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