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 48458U 26145.53284796 +.00000000 +00000-0 +47157-4 0 00002
2 48458 53.1577 181.3618 0001241 83.8171 276.2972 15.31703729 06
| Epoch (UTC): | 25 May 2026 12:47:18 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.3618° |
| argument of perigee: | 83.8171° |
| revolutions per day: | 15.31703729 |
| mean anomaly at epoch: | 276.2972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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