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 48213U 26145.39598047 +.00000000 +00000-0 +73078-3 0 00002
2 48213 87.8946 294.2404 0001594 111.6915 248.4385 13.14501676 08
| Epoch (UTC): | 25 May 2026 09:30:12 |
| Eccentricity: | 0.0001594 |
| inclination: | 87.8946° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2404° |
| argument of perigee: | 111.6915° |
| revolutions per day: | 13.14501676 |
| mean anomaly at epoch: | 248.4385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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