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 10489U 26053.81718909 +.00000000 +00000-0 +00000-0 0 00004
2 10489 5.3633 282.4389 0010615 82.8851 93.5138 1.00286947 01
| Epoch (UTC): | 22 February 2026 19:36:45 |
| Eccentricity: | 0.0010615 |
| inclination: | 5.3633° |
| perigee height: | 35738 km |
| apogee height: | 35827 km |
| right ascension of ascending node: | 282.4389° |
| argument of perigee: | 82.8851° |
| revolutions per day: | 1.00286947 |
| mean anomaly at epoch: | 93.5138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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