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 48095U 26145.44549084 +.00000000 +00000-0 +15900-4 0 00004
2 48095 53.1598 168.4653 0001142 91.9407 268.1725 15.31698073 04
| Epoch (UTC): | 25 May 2026 10:41:30 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.4653° |
| argument of perigee: | 91.9407° |
| revolutions per day: | 15.31698073 |
| mean anomaly at epoch: | 268.1725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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