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 48670U 26145.17888503 +.00000000 +00000-0 +25521-4 0 00005
2 48670 53.1572 108.4461 0001080 92.5087 267.6038 15.31703450 05
| Epoch (UTC): | 25 May 2026 04:17:35 |
| Eccentricity: | 0.0001080 |
| inclination: | 53.1572° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 108.4461° |
| argument of perigee: | 92.5087° |
| revolutions per day: | 15.31703450 |
| mean anomaly at epoch: | 267.6038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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