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 26145.23757896 +.00000000 +00000-0 +00000-0 0 00001
2 37481 4.4866 53.1296 0002190 3.0317 323.9988 1.00272123 05
| Epoch (UTC): | 25 May 2026 05:42:06 |
| Eccentricity: | 0.0002190 |
| inclination: | 4.4866° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 53.1296° |
| argument of perigee: | 3.0317° |
| revolutions per day: | 1.00272123 |
| mean anomaly at epoch: | 323.9988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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