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 46610U 26145.60719279 +.00000000 +00000-0 +00000-0 0 00009
2 46610 0.4649 84.9884 0041619 123.0689 11.9631 1.00271294 00
| Epoch (UTC): | 25 May 2026 14:34:21 |
| Eccentricity: | 0.0041619 |
| inclination: | 0.4649° |
| perigee height: | 35611 km |
| apogee height: | 35962 km |
| right ascension of ascending node: | 84.9884° |
| argument of perigee: | 123.0689° |
| revolutions per day: | 1.00271294 |
| mean anomaly at epoch: | 11.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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