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 46076U 26145.61626488 +.00000000 +00000-0 -10225-4 0 00000
2 46076 53.1614 103.4960 0001226 93.2647 266.8495 15.31711552 01
| Epoch (UTC): | 25 May 2026 14:47:25 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 103.4960° |
| argument of perigee: | 93.2647° |
| revolutions per day: | 15.31711552 |
| mean anomaly at epoch: | 266.8495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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