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 46696U 26145.58335647 +.00000000 +00000-0 +10108-2 0 00005
2 46696 53.0303 156.1559 0010563 20.9433 279.4117 15.91900115 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0010563 |
| inclination: | 53.0303° |
| perigee height: | 290 km |
| apogee height: | 304 km |
| right ascension of ascending node: | 156.1559° |
| argument of perigee: | 20.9433° |
| revolutions per day: | 15.91900115 |
| mean anomaly at epoch: | 279.4117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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