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 46141U 26145.49176299 +.00000000 +00000-0 +10812-2 0 00008
2 46141 53.0360 221.6005 0006314 345.8094 14.2738 15.56944734 01
| Epoch (UTC): | 25 May 2026 11:48:08 |
| Eccentricity: | 0.0006314 |
| inclination: | 53.0360° |
| perigee height: | 392 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 221.6005° |
| argument of perigee: | 345.8094° |
| revolutions per day: | 15.56944734 |
| mean anomaly at epoch: | 14.2738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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