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 40099U 26137.17006497 +.00000000 +00000-0 +00000-0 0 00008
2 40099 5.4224 75.6118 0001747 67.9613 149.1602 0.96774452 07
| Epoch (UTC): | 17 May 2026 04:04:53 |
| Eccentricity: | 0.0001747 |
| inclination: | 5.4224° |
| perigee height: | 36789 km |
| apogee height: | 36804 km |
| right ascension of ascending node: | 75.6118° |
| argument of perigee: | 67.9613° |
| revolutions per day: | 0.96774452 |
| mean anomaly at epoch: | 149.1602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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