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 37602U 26145.57124838 +.00000000 +00000-0 +00000-0 0 00007
2 37602 0.0157 2.1633 0002469 58.1613 325.5022 1.00272179 01
| Epoch (UTC): | 25 May 2026 13:42:35 |
| Eccentricity: | 0.0002469 |
| inclination: | 0.0157° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 2.1633° |
| argument of perigee: | 58.1613° |
| revolutions per day: | 1.00272179 |
| mean anomaly at epoch: | 325.5022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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