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 39088U 26106.74270449 +.00000000 +00000-0 +36511-4 0 00003
2 39088 98.4247 287.6607 0012349 74.1085 286.1461 14.35223791 09
| Epoch (UTC): | 16 April 2026 17:49:29 |
| Eccentricity: | 0.0012349 |
| inclination: | 98.4247° |
| perigee height: | 765 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 287.6607° |
| argument of perigee: | 74.1085° |
| revolutions per day: | 14.35223791 |
| mean anomaly at epoch: | 286.1461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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