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 26145.49844846 +.00000000 +00000-0 +99122-4 0 00006
2 39090 98.3917 326.2922 0007551 303.5977 56.4488 14.37147743 04
| Epoch (UTC): | 25 May 2026 11:57:45 |
| Eccentricity: | 0.0007551 |
| inclination: | 98.3917° |
| perigee height: | 763 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 326.2922° |
| argument of perigee: | 303.5977° |
| revolutions per day: | 14.37147743 |
| mean anomaly at epoch: | 56.4488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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