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 48454U 26145.37860979 +.00000000 +00000-0 -15057-4 0 00008
2 48454 53.1584 181.4058 0001173 94.5964 265.5172 15.31711834 01
| Epoch (UTC): | 25 May 2026 09:05:11 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.4058° |
| argument of perigee: | 94.5964° |
| revolutions per day: | 15.31711834 |
| mean anomaly at epoch: | 265.5172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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