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 26137.76217279 +.00000000 +00000-0 +29289-3 0 00007
2 40025 98.0972 146.7868 0007857 341.5889 18.5058 15.17749645 09
| Epoch (UTC): | 17 May 2026 18:17:31 |
| Eccentricity: | 0.0007857 |
| inclination: | 98.0972° |
| perigee height: | 507 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 146.7868° |
| argument of perigee: | 341.5889° |
| revolutions per day: | 15.17749645 |
| mean anomaly at epoch: | 18.5058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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