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 26073.51504617 +.00000000 +00000-0 +84680-3 0 00004
2 40074 98.4236 66.9687 0003219 103.9825 256.1761 15.11913095 07
| Epoch (UTC): | 14 March 2026 12:21:39 |
| Eccentricity: | 0.0003219 |
| inclination: | 98.4236° |
| perigee height: | 528 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 66.9687° |
| argument of perigee: | 103.9825° |
| revolutions per day: | 15.11913095 |
| mean anomaly at epoch: | 256.1761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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