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 48215U 26145.40709294 +.00000000 +00000-0 +63171-3 0 00007
2 48215 87.8933 294.2561 0001805 105.1645 254.9685 13.14503687 02
| Epoch (UTC): | 25 May 2026 09:46:12 |
| Eccentricity: | 0.0001805 |
| inclination: | 87.8933° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2561° |
| argument of perigee: | 105.1645° |
| revolutions per day: | 13.14503687 |
| mean anomaly at epoch: | 254.9685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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