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 48379U 26145.30338406 +.00000000 +00000-0 +17159-3 0 00005
2 48379 53.1601 349.4161 0001151 85.6204 274.4929 15.31691644 07
| Epoch (UTC): | 25 May 2026 07:16:52 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 349.4161° |
| argument of perigee: | 85.6204° |
| revolutions per day: | 15.31691644 |
| mean anomaly at epoch: | 274.4929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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