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 48214U 26145.64652529 +.00000000 +00000-0 +49777-3 0 00006
2 48214 87.8948 294.1892 0000958 105.7216 254.4020 13.14501314 04
| Epoch (UTC): | 25 May 2026 15:30:59 |
| Eccentricity: | 0.0000958 |
| inclination: | 87.8948° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.1892° |
| argument of perigee: | 105.7216° |
| revolutions per day: | 13.14501314 |
| mean anomaly at epoch: | 254.4020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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