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 26087.78078808 +.00000000 +00000-0 +13860-3 0 00004
2 39090 98.3903 269.9991 0009793 109.4666 250.7580 14.37110554 08
| Epoch (UTC): | 28 March 2026 18:44:20 |
| Eccentricity: | 0.0009793 |
| inclination: | 98.3903° |
| perigee height: | 761 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 269.9991° |
| argument of perigee: | 109.4666° |
| revolutions per day: | 14.37110554 |
| mean anomaly at epoch: | 250.7580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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