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 26144.45411132 +.00000000 +00000-0 +83831-4 0 00009
2 39090 98.3917 325.2736 0007587 307.1154 52.9339 14.37146928 02
| Epoch (UTC): | 24 May 2026 10:53:55 |
| Eccentricity: | 0.0007587 |
| inclination: | 98.3917° |
| perigee height: | 763 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 325.2736° |
| argument of perigee: | 307.1154° |
| revolutions per day: | 14.37146928 |
| mean anomaly at epoch: | 52.9339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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