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 26073.43811536 +.00000000 +00000-0 +15431-3 0 00000
2 39090 98.3892 256.0118 0009274 148.2913 211.8834 14.37099499 07
| Epoch (UTC): | 14 March 2026 10:30:53 |
| Eccentricity: | 0.0009274 |
| inclination: | 98.3892° |
| perigee height: | 761 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 256.0118° |
| argument of perigee: | 148.2913° |
| revolutions per day: | 14.37099499 |
| mean anomaly at epoch: | 211.8834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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