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 48094U 26145.52932117 +.00000000 +00000-0 +52602-2 0 00003
2 48094 53.1593 168.3533 0001424 77.3200 282.7960 15.31094184 02
| Epoch (UTC): | 25 May 2026 12:42:13 |
| Eccentricity: | 0.0001424 |
| inclination: | 53.1593° |
| perigee height: | 472 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 168.3533° |
| argument of perigee: | 77.3200° |
| revolutions per day: | 15.31094184 |
| mean anomaly at epoch: | 282.7960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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