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 40025U 26134.99315497 +.00000000 +00000-0 +26846-3 0 00006
2 40025 98.0977 143.8254 0008142 351.7406 8.3691 15.17718628 04
| Epoch (UTC): | 14 May 2026 23:50:08 |
| Eccentricity: | 0.0008142 |
| inclination: | 98.0977° |
| perigee height: | 507 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 143.8254° |
| argument of perigee: | 351.7406° |
| revolutions per day: | 15.17718628 |
| mean anomaly at epoch: | 8.3691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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