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 48438U 26145.37397095 +.00000000 +00000-0 +57180-4 0 00006
2 48438 53.1579 181.5489 0001128 84.7437 275.3693 15.31701477 01
| Epoch (UTC): | 25 May 2026 08:58:31 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.5489° |
| argument of perigee: | 84.7437° |
| revolutions per day: | 15.31701477 |
| mean anomaly at epoch: | 275.3693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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