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 26144.96032345 +.00000000 +00000-0 +45120-3 0 00002
2 40074 98.4238 145.8004 0000813 154.4681 205.6588 15.13112130 06
| Epoch (UTC): | 24 May 2026 23:02:51 |
| Eccentricity: | 0.0000813 |
| inclination: | 98.4238° |
| perigee height: | 526 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 145.8004° |
| argument of perigee: | 154.4681° |
| revolutions per day: | 15.13112130 |
| mean anomaly at epoch: | 205.6588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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