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 40730U 26145.28565388 +.00000000 +00000-0 +00000-0 0 00000
2 40730 54.0008 268.0305 0115020 30.1303 330.5127 2.00557419 00
| Epoch (UTC): | 25 May 2026 06:51:20 |
| Eccentricity: | 0.0115020 |
| inclination: | 54.0008° |
| perigee height: | 19877 km |
| apogee height: | 20488 km |
| right ascension of ascending node: | 268.0305° |
| argument of perigee: | 30.1303° |
| revolutions per day: | 2.00557419 |
| mean anomaly at epoch: | 330.5127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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