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 40028U 26138.81885067 +.00000000 +00000-0 +21039-3 0 00008
2 40028 98.0994 147.7855 0005081 301.9549 58.1187 15.14820151 05
| Epoch (UTC): | 18 May 2026 19:39:08 |
| Eccentricity: | 0.0005081 |
| inclination: | 98.0994° |
| perigee height: | 518 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 147.7855° |
| argument of perigee: | 301.9549° |
| revolutions per day: | 15.14820151 |
| mean anomaly at epoch: | 58.1187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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