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 48380U 26144.98642926 +.00000000 +00000-0 +17575-3 0 00007
2 48380 53.1601 350.7711 0001122 84.7141 275.3989 15.31714988 06
| Epoch (UTC): | 24 May 2026 23:40:27 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 350.7711° |
| argument of perigee: | 84.7141° |
| revolutions per day: | 15.31714988 |
| mean anomaly at epoch: | 275.3989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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