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 26101.24008159 +.00000000 +00000-0 +38889-3 0 00006
2 40074 98.4254 97.5398 0002863 66.9588 293.1941 15.12519713 05
| Epoch (UTC): | 11 April 2026 05:45:43 |
| Eccentricity: | 0.0002863 |
| inclination: | 98.4254° |
| perigee height: | 527 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 97.5398° |
| argument of perigee: | 66.9588° |
| revolutions per day: | 15.12519713 |
| mean anomaly at epoch: | 293.1941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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