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 40267U 26110.88893311 +.00000000 +00000-0 +00000-0 0 00003
2 40267 0.0346 78.0728 0000763 280.9193 310.6545 1.00272810 09
| Epoch (UTC): | 20 April 2026 21:20:03 |
| Eccentricity: | 0.0000763 |
| inclination: | 0.0346° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 78.0728° |
| argument of perigee: | 280.9193° |
| revolutions per day: | 1.00272810 |
| mean anomaly at epoch: | 310.6545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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