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 48211U 26145.39280338 +.00000000 +00000-0 +58416-3 0 00000
2 48211 87.8952 294.2442 0001036 87.7458 272.3791 13.14501694 08
| Epoch (UTC): | 25 May 2026 09:25:38 |
| Eccentricity: | 0.0001036 |
| inclination: | 87.8952° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2442° |
| argument of perigee: | 87.7458° |
| revolutions per day: | 13.14501694 |
| mean anomaly at epoch: | 272.3791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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