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 46335U 26145.62430308 +.00000000 +00000-0 +10176-2 0 00005
2 46335 53.0268 307.8997 0012911 287.2857 72.6764 16.12624063 06
| Epoch (UTC): | 25 May 2026 14:58:59 |
| Eccentricity: | 0.0012911 |
| inclination: | 53.0268° |
| perigee height: | 231 km |
| apogee height: | 248 km |
| right ascension of ascending node: | 307.8997° |
| argument of perigee: | 287.2857° |
| revolutions per day: | 16.12624063 |
| mean anomaly at epoch: | 72.6764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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