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 46461U 26145.60975293 +.00000000 +00000-0 +99275-3 0 00008
2 46461 97.2182 206.4320 0007950 173.5622 186.5759 15.97896148 05
| Epoch (UTC): | 25 May 2026 14:38:02 |
| Eccentricity: | 0.0007950 |
| inclination: | 97.2182° |
| perigee height: | 275 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 206.4320° |
| argument of perigee: | 173.5622° |
| revolutions per day: | 15.97896148 |
| mean anomaly at epoch: | 186.5759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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