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 26067.68492177 +.00000000 +00000-0 +23873-3 0 00007
2 23657 82.5244 137.7633 0017206 303.2211 56.7360 14.94362384 09
| Epoch (UTC): | 08 March 2026 16:26:17 |
| Eccentricity: | 0.0017206 |
| inclination: | 82.5244° |
| perigee height: | 572 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 137.7633° |
| argument of perigee: | 303.2211° |
| revolutions per day: | 14.94362384 |
| mean anomaly at epoch: | 56.7360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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