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 54837U 26146.09274193 +.00000000 +00000-0 +47067-3 0 00001
2 54837 42.9869 34.7937 0008486 265.2687 94.7237 16.40586181 04
| Epoch (UTC): | 26 May 2026 02:13:32 |
| Eccentricity: | 0.0008486 |
| inclination: | 42.9869° |
| perigee height: | 159 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 34.7937° |
| argument of perigee: | 265.2687° |
| revolutions per day: | 16.40586181 |
| mean anomaly at epoch: | 94.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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