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 40015U 26118.73810240 +.00000000 +00000-0 +16117-3 0 00005
2 40015 97.6374 283.7856 0033597 155.1840 205.1000 14.85275953 05
| Epoch (UTC): | 28 April 2026 17:42:52 |
| Eccentricity: | 0.0033597 |
| inclination: | 97.6374° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 283.7856° |
| argument of perigee: | 155.1840° |
| revolutions per day: | 14.85275953 |
| mean anomaly at epoch: | 205.1000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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