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 48691U 26145.11072950 +.00000000 +00000-0 +62175-4 0 00009
2 48691 53.1592 79.8703 0000955 90.1708 269.9403 15.31703425 07
| Epoch (UTC): | 25 May 2026 02:39:27 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 79.8703° |
| argument of perigee: | 90.1708° |
| revolutions per day: | 15.31703425 |
| mean anomaly at epoch: | 269.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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