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 46537U 26145.34163693 +.00000000 +00000-0 +71460-3 0 00002
2 46537 53.0441 127.5643 0005231 17.4111 342.7079 15.59794105 06
| Epoch (UTC): | 25 May 2026 08:11:57 |
| Eccentricity: | 0.0005231 |
| inclination: | 53.0441° |
| perigee height: | 385 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 127.5643° |
| argument of perigee: | 17.4111° |
| revolutions per day: | 15.59794105 |
| mean anomaly at epoch: | 342.7079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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