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 37481U 26146.23570948 +.00000000 +00000-0 +00000-0 0 00003
2 37481 4.4888 53.1297 0002159 3.3471 323.9943 1.00272323 02
| Epoch (UTC): | 26 May 2026 05:39:25 |
| Eccentricity: | 0.0002159 |
| inclination: | 4.4888° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 53.1297° |
| argument of perigee: | 3.3471° |
| revolutions per day: | 1.00272323 |
| mean anomaly at epoch: | 323.9943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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