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 26156.71854375 +.00000000 +00000-0 +30597-3 0 00004
2 40028 98.0990 166.8498 0005479 222.0815 137.9996 15.15075711 05
| Epoch (UTC): | 05 June 2026 17:14:42 |
| Eccentricity: | 0.0005479 |
| inclination: | 98.0990° |
| perigee height: | 517 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 166.8498° |
| argument of perigee: | 222.0815° |
| revolutions per day: | 15.15075711 |
| mean anomaly at epoch: | 137.9996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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