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 02411U 26151.80828714 +.00000000 +00000-0 -94661-2 0 00003
2 02411 90.3353 277.2466 0011654 75.1080 285.1061 8.59615314 00
| Epoch (UTC): | 31 May 2026 19:23:56 |
| Eccentricity: | 0.0011654 |
| inclination: | 90.3353° |
| perigee height: | 3676 km |
| apogee height: | 3700 km |
| right ascension of ascending node: | 277.2466° |
| argument of perigee: | 75.1080° |
| revolutions per day: | 8.59615314 |
| mean anomaly at epoch: | 285.1061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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