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 46034U 26145.23130294 +.00000000 +00000-0 +57358-4 0 00004
2 46034 53.1613 131.1832 0001325 82.8143 277.3008 15.30197926 04
| Epoch (UTC): | 25 May 2026 05:33:04 |
| Eccentricity: | 0.0001325 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.1832° |
| argument of perigee: | 82.8143° |
| revolutions per day: | 15.30197926 |
| mean anomaly at epoch: | 277.3008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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