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 40277U 26146.02203786 +.00000000 +00000-0 +00000-0 0 00000
2 40277 0.0155 284.6253 0000471 208.9844 170.9297 1.00272358 03
| Epoch (UTC): | 26 May 2026 00:31:44 |
| Eccentricity: | 0.0000471 |
| inclination: | 0.0155° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 284.6253° |
| argument of perigee: | 208.9844° |
| revolutions per day: | 1.00272358 |
| mean anomaly at epoch: | 170.9297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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