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 40748U 26143.62365684 +.00000000 +00000-0 +00000-0 0 00002
2 40748 54.8929 302.8909 0007596 263.8817 96.0113 1.86231735 01
| Epoch (UTC): | 23 May 2026 14:58:03 |
| Eccentricity: | 0.0007596 |
| inclination: | 54.8929° |
| perigee height: | 21507 km |
| apogee height: | 21549 km |
| right ascension of ascending node: | 302.8909° |
| argument of perigee: | 263.8817° |
| revolutions per day: | 1.86231735 |
| mean anomaly at epoch: | 96.0113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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