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 66848U 26145.07409644 +.00000000 +00000-0 +49838-3 0 00002
2 66848 43.0049 272.4382 0003981 267.9174 92.1222 15.27590100 07
| Epoch (UTC): | 25 May 2026 01:46:41 |
| Eccentricity: | 0.0003981 |
| inclination: | 43.0049° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 272.4382° |
| argument of perigee: | 267.9174° |
| revolutions per day: | 15.27590100 |
| mean anomaly at epoch: | 92.1222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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