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 26151.72802145 +.00000000 +00000-0 +00000-0 0 00001
2 39237 0.0092 86.6679 0002647 322.4828 167.1594 1.00272004 06
| Epoch (UTC): | 31 May 2026 17:28:21 |
| Eccentricity: | 0.0002647 |
| inclination: | 0.0092° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 86.6679° |
| argument of perigee: | 322.4828° |
| revolutions per day: | 1.00272004 |
| mean anomaly at epoch: | 167.1594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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