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 48295U 26145.23693172 +.00000000 +00000-0 -71491-4 0 00009
2 48295 53.1623 79.5067 0001589 112.4447 247.6723 15.31715775 03
| Epoch (UTC): | 25 May 2026 05:41:10 |
| Eccentricity: | 0.0001589 |
| inclination: | 53.1623° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 79.5067° |
| argument of perigee: | 112.4447° |
| revolutions per day: | 15.31715775 |
| mean anomaly at epoch: | 247.6723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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