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 40100U 26143.48081596 +.00000000 +00000-0 +00000-0 0 00005
2 40100 4.6539 76.4522 0002395 286.9907 307.7168 0.99127425 01
| Epoch (UTC): | 23 May 2026 11:32:22 |
| Eccentricity: | 0.0002395 |
| inclination: | 4.6539° |
| perigee height: | 36100 km |
| apogee height: | 36121 km |
| right ascension of ascending node: | 76.4522° |
| argument of perigee: | 286.9907° |
| revolutions per day: | 0.99127425 |
| mean anomaly at epoch: | 307.7168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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