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 48381U 26145.54699845 +.00000000 +00000-0 +42989-4 0 00001
2 48381 53.1619 350.7941 0001277 82.1630 277.9516 15.30184130 00
| Epoch (UTC): | 25 May 2026 13:07:40 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1619° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.7941° |
| argument of perigee: | 82.1630° |
| revolutions per day: | 15.30184130 |
| mean anomaly at epoch: | 277.9516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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