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 46156U 26145.58335647 +.00000000 +00000-0 +83128-3 0 00009
2 46156 53.0411 238.1757 0005447 311.5710 127.8825 15.78414446 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005447 |
| inclination: | 53.0411° |
| perigee height: | 331 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 238.1757° |
| argument of perigee: | 311.5710° |
| revolutions per day: | 15.78414446 |
| mean anomaly at epoch: | 127.8825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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