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 46348U 26145.15048537 +.00000000 +00000-0 +67533-3 0 00006
2 46348 53.0368 306.1703 0002849 60.6075 299.5213 15.40519884 05
| Epoch (UTC): | 25 May 2026 03:36:41 |
| Eccentricity: | 0.0002849 |
| inclination: | 53.0368° |
| perigee height: | 443 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 306.1703° |
| argument of perigee: | 60.6075° |
| revolutions per day: | 15.40519884 |
| mean anomaly at epoch: | 299.5213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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