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 48684U 26145.54020002 +.00000000 +00000-0 +56265-4 0 00002
2 48684 53.1590 80.4781 0001180 86.2747 273.8389 15.31707891 09
| Epoch (UTC): | 25 May 2026 12:57:53 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 80.4781° |
| argument of perigee: | 86.2747° |
| revolutions per day: | 15.31707891 |
| mean anomaly at epoch: | 273.8389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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