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 40071U 26138.81205778 +.00000000 +00000-0 +54356-4 0 00000
2 40071 98.3854 98.7375 0007676 19.0424 341.1077 14.89881533 09
| Epoch (UTC): | 18 May 2026 19:29:21 |
| Eccentricity: | 0.0007676 |
| inclination: | 98.3854° |
| perigee height: | 593 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 98.7375° |
| argument of perigee: | 19.0424° |
| revolutions per day: | 14.89881533 |
| mean anomaly at epoch: | 341.1077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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