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 40074U 26069.94109529 +.00000000 +00000-0 +70731-3 0 00001
2 40074 98.4235 63.0304 0003042 110.4993 249.6561 15.11824757 04
| Epoch (UTC): | 10 March 2026 22:35:10 |
| Eccentricity: | 0.0003042 |
| inclination: | 98.4235° |
| perigee height: | 529 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 63.0304° |
| argument of perigee: | 110.4993° |
| revolutions per day: | 15.11824757 |
| mean anomaly at epoch: | 249.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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