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 26098.92460557 +.00000000 +00000-0 +46360-3 0 00003
2 40074 98.4253 94.9852 0002875 69.3282 290.8254 15.12482054 09
| Epoch (UTC): | 08 April 2026 22:11:25 |
| Eccentricity: | 0.0002875 |
| inclination: | 98.4253° |
| perigee height: | 527 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 94.9852° |
| argument of perigee: | 69.3282° |
| revolutions per day: | 15.12482054 |
| mean anomaly at epoch: | 290.8254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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