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 48232U 26145.41342594 +.00000000 +00000-0 +53584-3 0 00000
2 48232 87.8952 294.2382 0001889 104.9891 255.1448 13.14501638 09
| Epoch (UTC): | 25 May 2026 09:55:20 |
| Eccentricity: | 0.0001889 |
| inclination: | 87.8952° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2382° |
| argument of perigee: | 104.9891° |
| revolutions per day: | 13.14501638 |
| mean anomaly at epoch: | 255.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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