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 40202U 26108.92242238 +.00000000 +00000-0 +34258-2 0 00004
2 40202 19.9108 217.0100 7105826 154.7714 271.2740 2.36474766 05
| Epoch (UTC): | 18 April 2026 22:08:17 |
| Eccentricity: | 0.7105826 |
| inclination: | 19.9108° |
| perigee height: | 509 km |
| apogee height: | 34331 km |
| right ascension of ascending node: | 217.0100° |
| argument of perigee: | 154.7714° |
| revolutions per day: | 2.36474766 |
| mean anomaly at epoch: | 271.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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