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 26064.67171344 +.00000000 +00000-0 +25849-3 0 00008
2 23657 82.5252 140.6322 0017356 314.0532 45.9259 14.94347513 02
| Epoch (UTC): | 05 March 2026 16:07:16 |
| Eccentricity: | 0.0017356 |
| inclination: | 82.5252° |
| perigee height: | 572 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 140.6322° |
| argument of perigee: | 314.0532° |
| revolutions per day: | 14.94347513 |
| mean anomaly at epoch: | 45.9259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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