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 39090U 26072.46336656 +.00000000 +00000-0 +16028-3 0 00000
2 39090 98.3892 255.0613 0009238 151.0147 209.1554 14.37098624 05
| Epoch (UTC): | 13 March 2026 11:07:14 |
| Eccentricity: | 0.0009238 |
| inclination: | 98.3892° |
| perigee height: | 761 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 255.0613° |
| argument of perigee: | 151.0147° |
| revolutions per day: | 14.37098624 |
| mean anomaly at epoch: | 209.1554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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