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 39237U 26145.52536509 +.00000000 +00000-0 +00000-0 0 00000
2 39237 0.0119 291.7113 0002812 112.0350 93.5063 1.00270748 01
| Epoch (UTC): | 25 May 2026 12:36:31 |
| Eccentricity: | 0.0002812 |
| inclination: | 0.0119° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 291.7113° |
| argument of perigee: | 112.0350° |
| revolutions per day: | 1.00270748 |
| mean anomaly at epoch: | 93.5063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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