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 48668U 26145.61695682 +.00000000 +00000-0 +91919-4 0 00009
2 48668 53.1606 106.1530 0001333 89.4780 270.6374 15.31710403 01
| Epoch (UTC): | 25 May 2026 14:48:25 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 106.1530° |
| argument of perigee: | 89.4780° |
| revolutions per day: | 15.31710403 |
| mean anomaly at epoch: | 270.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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