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 26031.85947556 +.00000000 +00000-0 +23178-3 0 00001
2 23657 82.5254 171.8649 0019838 63.4013 296.9238 14.94191642 03
| Epoch (UTC): | 31 January 2026 20:37:38 |
| Eccentricity: | 0.0019838 |
| inclination: | 82.5254° |
| perigee height: | 571 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 171.8649° |
| argument of perigee: | 63.4013° |
| revolutions per day: | 14.94191642 |
| mean anomaly at epoch: | 296.9238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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