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 40079U 26145.31830731 +.00000000 +00000-0 +00000-0 0 00007
2 40079 0.0494 354.6089 0001904 130.8686 234.5398 5.00115672 01
| Epoch (UTC): | 25 May 2026 07:38:21 |
| Eccentricity: | 0.0001904 |
| inclination: | 0.0494° |
| perigee height: | 8063 km |
| apogee height: | 8069 km |
| right ascension of ascending node: | 354.6089° |
| argument of perigee: | 130.8686° |
| revolutions per day: | 5.00115672 |
| mean anomaly at epoch: | 234.5398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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