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 46478U 26145.59911483 +.00000000 +00000-0 +16600-3 0 00006
2 46478 97.8823 224.5043 0003242 5.7926 354.3321 14.76579987 02
| Epoch (UTC): | 25 May 2026 14:22:43 |
| Eccentricity: | 0.0003242 |
| inclination: | 97.8823° |
| perigee height: | 638 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 224.5043° |
| argument of perigee: | 5.7926° |
| revolutions per day: | 14.76579987 |
| mean anomaly at epoch: | 354.3321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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