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 46479U 26145.63570023 +.00000000 +00000-0 +81223-4 0 00007
2 46479 97.8885 225.5445 0001148 80.8411 279.2929 14.76523071 06
| Epoch (UTC): | 25 May 2026 15:15:24 |
| Eccentricity: | 0.0001148 |
| inclination: | 97.8885° |
| perigee height: | 640 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 225.5445° |
| argument of perigee: | 80.8411° |
| revolutions per day: | 14.76523071 |
| mean anomaly at epoch: | 279.2929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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