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 26087.92169674 +.00000000 +00000-0 +13063-1 0 00002
2 02411 90.3253 276.5112 0011705 135.8172 224.3616 8.59615546 00
| Epoch (UTC): | 28 March 2026 22:07:14 |
| Eccentricity: | 0.0011705 |
| inclination: | 90.3253° |
| perigee height: | 3676 km |
| apogee height: | 3700 km |
| right ascension of ascending node: | 276.5112° |
| argument of perigee: | 135.8172° |
| revolutions per day: | 8.59615546 |
| mean anomaly at epoch: | 224.3616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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