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 48238U 26145.38645984 +.00000000 +00000-0 +32010-3 0 00002
2 48238 87.8941 294.2459 0001854 84.0913 276.0428 13.14501687 07
| Epoch (UTC): | 25 May 2026 09:16:30 |
| Eccentricity: | 0.0001854 |
| inclination: | 87.8941° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2459° |
| argument of perigee: | 84.0913° |
| revolutions per day: | 13.14501687 |
| mean anomaly at epoch: | 276.0428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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